appendix a - freetraxanh.free.fr/download/metallic materials properties development … · mmpds 31...

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MMPDS 31 January 2003 A-1 A.0 GLOSSARY A.1 ABBREVIATIONS a Amplitude; crack or flaw dimension; measure of flaw size, inches. a c Critical half crack length. a o Initial half crack length. A Area of cross section, square inches; ratio of alternating stress to mean stress; subscript “axial”; A basis for mechanical-property values (see Section 1.4.1.1 or Section 9.1.6); “A” ratio, loading amplitude/mean load; or area. A ε Strain “A” ratio, strain amplitude/mean strain. A i Model parameter. AD — Anderson-Darling test statistic, computed in goodness-of-fit tests for normality or Weibullness. AISI American Iron and Steel Institute. AMS Aerospace Materials Specification (published by Society of Automotive Engineers, Inc.). Ann — Annealed. AN Air Force-Navy Aeronautical Standard. ASTM American Society for Testing and Materials. b Width of sections; subscript “bending”. br Subscript “bearing”. B Biaxial ratio (see Equation 1.3.2.(h)); B-basis for mechanical-property values (see Section 1.4.1.1 or Section 9.1.6). Btu British thermal unit(s). BUS Individual or typical bearing ultimate strength. BYS Individual or typical bearing yield strength. c Fixity coefficient for columns; subscript “compression”. cpm Cycles per minute. C Specific heat; Celsius; Constant. CEM Consumable electrode melted. CRES Corrosion resistant steel (stainless steel). C(T) Compact tension. CYS Individual or typical compressive yield strength. d Mathematical operator denoting differential. D or d Diameter, or Durbin Watson statistic; hole or fastener diameter; dimpled hole. df Degrees of freedom. e Elongation in percent, a measure of the ductility of a material based on a tension test; unit deformation or strain; subscript “fatigue or endurance”; the minimum distance from a hole, center to the edge of the sheet; Engineering strain. e e Elastic strain. e p Plastic strain. e/D Ratio of edge distance (center of the hole to edge of the sheet) to hole diameter (bearing strength). E Modulus of elasticity in tension or compression; average ratio of stress to strain for stress below proportional limit. APPENDIX A

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Page 1: APPENDIX A - Freetraxanh.free.fr/Download/Metallic Materials Properties Development … · MMPDS 31 January 2003 A-6 σx — Population standard deviation of x. x σ2 — Population

MMPDS31 January 2003

A-1

A.0 GLOSSARY

A.1 ABBREVIATIONS

a — Amplitude; crack or flaw dimension; measure of flaw size, inches.ac — Critical half crack length.ao — Initial half crack length.A — Area of cross section, square inches; ratio of alternating stress to mean stress; subscript

“axial”; A basis for mechanical-property values (see Section 1.4.1.1 or Section 9.1.6); “A”ratio, loading amplitude/mean load; or area.

Aε — Strain “A” ratio, strain amplitude/mean strain.Ai — Model parameter.AD — Anderson-Darling test statistic, computed in goodness-of-fit tests for normality or

Weibullness.AISI — American Iron and Steel Institute.AMS — Aerospace Materials Specification (published by Society of Automotive Engineers, Inc.).Ann — Annealed.AN — Air Force-Navy Aeronautical Standard.ASTM — American Society for Testing and Materials.b — Width of sections; subscript “bending”.br — Subscript “bearing”.B — Biaxial ratio (see Equation 1.3.2.(h)); B-basis for mechanical-property values (see Section

1.4.1.1 or Section 9.1.6).Btu — British thermal unit(s).BUS — Individual or typical bearing ultimate strength.BYS — Individual or typical bearing yield strength.c — Fixity coefficient for columns; subscript “compression”.cpm — Cycles per minute.C — Specific heat; Celsius; Constant.CEM — Consumable electrode melted.CRES — Corrosion resistant steel (stainless steel).C(T) — Compact tension.CYS — Individual or typical compressive yield strength.d — Mathematical operator denoting differential.D or d — Diameter, or Durbin Watson statistic; hole or fastener diameter; dimpled hole.df — Degrees of freedom.e — Elongation in percent, a measure of the ductility of a material based on a tension test; unit

deformation or strain; subscript “fatigue or endurance”; the minimum distance from a hole,center to the edge of the sheet; Engineering strain.

ee — Elastic strain.ep — Plastic strain.e/D — Ratio of edge distance (center of the hole to edge of the sheet) to hole diameter (bearing

strength).E — Modulus of elasticity in tension or compression; average ratio of stress to strain for stress

below proportional limit.

APPENDIX A

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Ec — Modulus of elasticity in compression; average ratio of stress to strain below proportionallimit.

Es — Secant modulus of elasticity, Eq. 9.8.4.2(c).Et — Tangent modulus of elasticity.ELI — Extra low interstitial (grade of titanium alloy).ER — Equivalent round.ESR — Electro-slag remelted.f — Internal (or calculated) tension stress; stress applied to the gross flawed section; creep

stress.fb — Internal (or calculated) primary bending stress.fc — Internal (or calculated) compressive stress; maximum stress at fracture: gross stress limit

(for screening elastic fracture data).fpl — Proportional limit.fs — Internal (or calculated) shear stress.ft — Internal (or calculated) tensile stress.ft — Foot: feet.F — Design stress; Fahrenheit; Ratio of two sample variances.FA — Design axial stress.Fb — Design bending stress; modulus of rupture in bending.Fbru — Design ultimate bearing stress.Fbry — Design bearing yield stress.Fc — Design column stress.Fcc — Design crushing or crippling stress (upper limit of column stress for local failure).Fcu — Design ultimate compressive stress.Fcy — Design compressive yield stress at which permanent strain equals 0.002.FH — Design hoop stress.Fs — Design shear stress.Fsp — Design proportional limit in shear.Fst — Design modulus of rupture in torsion.Fsu — Design ultimate stress in pure shear (this value represents the average shear stress over the

cross section).Fsy — Design shear yield stress.Ftp — Design proportional limit in tension.Ftu — Design tensile ultimate stress.Fty — Design tensile yield stress at which permanent strain equals 0.002.g — Gram(s).G — Modulus of rigidity (shear modulus).Gpa — Gigapascal(s).hr — Hour(s).H — Subscript “hoop”.HIP — Hot isostatically pressed.i — Slope (due to bending) of neutral plane of a beam, in radians (1 radian = 57.3 degrees).in. — Inch(es).I — Axial moment of inertia.J — Torsion constant (= Ip for round tubes); Joule.k — Tolerance limit factor for the normal distribution and the specified probability, confidence,

and degrees of freedom; Strain at unit stress.k99, k90 — One-sided tolerance limit factor for T99 and T90, respectively (see Section 9.10.1 and

9.10.7).kA,B — k factor for A basis or B basis, respectively (see Section 9.10.1 and 9.10.7).ksi — Kips (1,000 pounds) per square inch.

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K — A constant, generally empirical; thermal conductivity; stress intensity; Kelvin; correctionfactor.

Kapp — Apparent plane stress fracture toughness or residual strength.Kc — Critical plane stress fracture toughness, a measure of fracture toughness at point of crack

growth instability.Kf — Fatigue notch factor, or fatigue strength reduction factor.KIc — Plane strain fracture toughness.KN — Empirically calculated fatigue notch factor.Kt — Theoretical stress concentration factor.lb — Pound.ln — Natural (base e) logarithm.log — Base 10 logarithm.L — Length; subscript “lateral”; longitudinal (grain direction).LT — Long transverse (grain direction).m — Subscript “mean”; metre; slope.mm — Millimeter(s).M — Applied moment or couple, usually a bending moment.Mc — Machine countersunk.Mg — Megagram(s).MIG — Metal-inert-gas (welding).MPa — Megapascal(s).MS — Military Standard.M.S. — Margin of safety.M(T) — Middle tension.n — Number of individual measurements or pairs of measurements; subscript “normal”; cycles

applied to failure; shape parameter for the standard stress-strain curve (Ramberg-Osgoodparameter); number of fatigue cycles endured.

N — Fatigue life, number of cycles to failure; Newton; normalized.Nf — Fatigue life, cycles to failure.Ni* — Fatigue life, cycles to initiation.Nt* — Transition fatigue life where plastic and elastic strains are equal.NAS — National Aerospace Standard.p — Subscript “polar”; subscript “proportional limit”.psi — Pounds per square inch.P — Load; applied load (total, not unit, load); exposure parameter; probability.Pa — Load amplitude.Pm — Mean load.Pmax — Maximum load.Pmin — Minimum load.Pu — Test ultimate load, pounds per fastener.Py — Test yield load, pounds per fastener.q — Fatigue notch sensitivity.Q — Static moment of a cross section.Q&T — Quenched and tempered.

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r — Radius; root radius; reduced ratio (regression analysis); ratio of two pair measurements;rank of test point within a sample.

— average ratio of paired measurements.rR — Load (stress) ratio, or residual (observed minus predicted value); stress ratio, ratio of

minimum stress to maximum stress in a fatigue cycle; reduced ratio.Rb — Stress ratio in bending.Rc — Stress ratio in compression; Rockwell hardness - C scale.Rε — Strain ratio, εmin/εmax.Rs — Stress ratio in shear or torsion; ratio of applied load to allowable shear load.Rt — Ratio of applied load to allowable tension load.RA — Reduction of area.R.H. — Relative humidity.RMS — Root-mean-square (surface finish).RT — Room temperature.s — Estimated population standard deviation; sample standard deviation; subscript “shear”.s2 — Sample variance.S — Shear force; nominal engineering stress, fatigue; S-basis for mechanical-property values

(see Section 1.4.1.1).Sa — Stress amplitude, fatigue.Se — Fatigue limit.Seq* — Equivalent stress.Sf — Fatigue limit.sm — Mean stress, fatigue.Smax — Highest algebraic value of stress in the stress cycle.Smin — Lowest algebraic value of stress in the stress cycle.Sr — Algebraic difference between the maximum and minimum stresses in one cycle.Sy — Root mean square error.SAE — Society of Automotive Engineers.SCC — Stress-corrosion cracking.SEE — Estimate population standard error of estimate.SR — Studentized residual.ST — Short transverse (grain direction).STA — Solution treated and aged.SUS — Individual or typical shear ultimate strength.SYS — Individual or typical shear yield strength.t — Thickness; subscript “tension”; exposure time; elapsed time; tolerance factor for the “t”

distribution with the specified probability and appropriate degrees of freedom.T — Transverse direction; applied torsional moment; transverse (grain direction); subscript

“transverse”.TF — Exposure temperature.T90 — Statistically based lower tolerance bound for a mechanical property such that at least

90 percent of the population is expected to exceed T90 with 95 percent confidence.T99 — Statistically based lower tolerance bound for a mechanical property such that at least

99 percent of the population is expected to exceed T99 with 95 percent confidence.TIG — Tungsten-inert-gas (welding).TUS — Individual or typical tensile ultimate strength.

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TUS (Su)* — Tensile ultimate strength.TYS — Individual or typical tensile yield strength.u — Subscript “ultimate”.U — Factor of utilization.V99,V90 — The tolerance limit factor corresponding to T99, T90 for the three-parameter Weibull

distribution, based on a 95 percent confidence level and a sample of size n.W — Width of center-through-cracked tension panel; Watt.

— Distance along a coordinate axis.xx — Sample mean based upon n observations.X — Value of an individual measurement; average value of individual measurements.y — Deflection (due to bending) of elastic curve of a beam; distance from neutral axis to given

fiber; subscript “yield”; distance along a coordinate axis.Y — Nondimensional factor relating component geometry and flaw size. See Reference

1.4.12.2.1(a) for values.z — Distance along a coordinate axis.Z — Section modulus, I/y.

A.2 SYMBOLS

α — (1) Coefficient of thermal expansion, mean; constant. (2) Significance level; probability(risk of erroneously rejecting the null hypothesis (see Section 9.5.3)).

α99, α90 — Shape parameter estimates for a T99 or T90 value based on an assumed three-parameterWeibull distribution.

α50 — Shape parameter estimate for the Anderson-Darling goodness-of-fit test based on anassumed three-parameter Weibull distribution.

β — Constant.β99, β90 — Scale parameter estimate for a T99 or T90 value based on an assumed three-parameter

Weibull distribution.β50 — Scale parameter estimate for the Anderson-Darling goodness-of-fit test based on an

assumed three-parameter Weibull distribution.∆ε or εr

* — strain range, εmax - εmin.∆εe — Elastic strain range.∆εp — Plastic strain range.∆S (Sr)* — Stress range.∆σ — True or local stress range.ε — True or local strain.εeq* — Equivalent strain.εm — Mean strain, (εmax + εmin)/2.εmax — Maximum strain.εmin — Minimum strain.εt — Total (elastic plus plastic) strain at failure determined from tensile stress-strain curve.δ — Deflection.Φ — Angular deflection.ρ — Radius of gyration; Neuber constant (block length).µ — Poisson’s ratio.

— True or local stress; or population standard deviation.σ

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x — Population standard deviation of x.σx

2 — Population variance of x.σ99, 90 — Threshold estimates for a T99 or T90 value based on an assumed three-parameter Weibullτ τ

distribution.50 — Threshold estimate for the Anderson-Darling goodness-of-fit test based on an assumedτ

three-parameter Weibull distribution. ω — Density; flank angle.4 — Infinity.G — The sum of.N — Superscript that denotes value determined by regression analysis.

A.3 DEFINITIONS

A-Basis.—The lower of either a statistically calculated number, or the specification minimum (S-basis).The statistically calculated number indicates that at least 99 percent of the population of values is expectedto equal or exceed the A-basis mechanical design property, with a confidence of 95 percent.

Alternating Load.—See Loading Amplitude.

B-Basis.—At least 90 percent of the population of values is expected to equal or exceed the B-basismechanical property allowable, with a confidence of 95 percent.

Cast.—Cast consists of the sequential ingots which are melted from a single furnace change and poured inone or more drops without changes in the processing parameters. (The cast number is for internalidentification and is not reported.) (See Table 9.2.4.2).

Casting.—One or more parts which are melted from a single furnace change and poured in one or moremolds without changes in the processing parameters. (The cast number is for internal identification and isnot reported.) (See Table 9.2.4.2).

Confidence.—A specified degree of certainty that at least a given proportion of all future measurements canbe expected to equal or exceed the lower tolerance limit. Degree of certainty is referred to as the confidencecoefficient. For MMPDS, the confidence coefficient is 95 percent which, as related to design properties,means that, in the long run over many future samples, 95 percent of conclusions regarding exceedance of Aand B-values would be true.

Confidence Interval.—An interval estimate of a population parameter computed so that the statement “thepopulation parameter lies in this interval” will be true, on the average, in a stated proportion of the timessuch statements are made.

Confidence Interval Estimate.—Range of values, computed with the sample that is expected to include thepopulation variance or mean.

Confidence Level (or Coefficient).—The stated portion of the time the confidence interval is expected toinclude the population parameter.

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A-7

Figure A.1. Typical creep-rupture curve.

Confidence Limits*.—The two numeric values that define a confidence interval.

Constant-Amplitude Loading.—A loading in which all of the peak loads are equal and all of the valley loadsare equal.

Constant-Life Fatigue Diagram.—A plot (usually on Cartesian coordinates) of a family of curves, each ofwhich is for a single fatigue life, N—relating S, Smax, and/or Smin to the mean stress, Sm. Generally, theconstant life fatigue diagram is derived from a family of S/N curves, each of which represents a differentstress ratio (A or R) for a 50 percent probability of survival. NOTE— MMPDS does not present fatiguedata in the form of constant-life diagrams.

Creep.—The time-dependent deformation of a solid resulting from force.

Note 1—Creep tests are usually made at constant load and temperature. For tests on metals, initialloading strain, however defined, is not included.

Note 2—This change in strain is sometimes referred to as creep strain.

Creep-Rupture Curve.—Results of material tests under constant load and temperature; usually plotted asstrain versus time to rupture. A typical plot of creep-rupture data is shown below. The strain indicated inthis curve includes both initial deformation due to loading and plastic strain due to creep.

Creep-Rupture Strength.—Stress that will cause fracture in a creep test at a given time, in a specifiedconstant environment. Note: This is sometimes referred to as the stress-rupture strength.

Creep-Rupture Test.—A creep-rupture test is one in which progressive specimen deformation and time forrupture are measured. In general, deformation is much larger than that developed during a creep test.

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A-8

Creep-Strain.—The time-dependent part of the strain resulting from stress, excluding initial loading strainand thermal expansion.

Creep Strength.—Stress that causes a given creep in a creep test at a given time in a specified constantenvironment.

Creep Stress.—The constant load divided by the original cross-sectional area of the specimen.

Creep Test.—A creep test has the objective of measuring deformation and deformation rates at stressesusually well below those which would result in fracture during the time of testing.

Critical Stress Intensity Factor.—A limiting value of the stress intensity factor beyond which continuedflaw propagation and/or fracture may be expected. This value is dependent on material and may vary withtype of loading and conditions of use.

Cycle.—Under constant-amplitude loading, the load varies from the minimum to the maximum and then tothe minimum load. The symbol n or N (see definition of fatigue life) is used to indicate the number ofcycles.

Deformable Shank Fasteners.—A fastener whose shank is deformed in the grip area during normalinstallation processes.

Degree of Freedom.—Number of degrees of freedom for n variables may be defined as number of variablesminus number of constraints between them. Since the standard deviation calculation contains one fixedvalue (the mean) it has n - 1 degrees of freedom.

Degrees of Freedom.—Number of independent comparisons afforded by a sample.

Discontinued Test.—See Runout.

Elapsed Time.—The time interval from application of the creep stress to a specified observation.

Fatigue.—The process of progressive localized permanent structural change occurring in a materialsubjected to conditions that produce fluctuating stresses and strains at some point or points, and which mayculminate in cracks or complete fracture after a sufficient number of fluctuations. NOTE—fluctuations instress and in time (frequency), as in the case of “random vibration.”

Fatigue Life.—N—the number of cycles of stress or strain of a specified character that a given specimensustains before failure of a specified nature occurs.

Fatigue Limit.—Sf—the limiting value of the median fatigue strength as N becomes very large. NOTE—-Certain materials and environments preclude the attainment of a fatigue limit. Values tabulated as “fatiguelimits” in the literature are frequently (but not always) values of SN for 50 percent survival at N cycles ofstress in which Sm = 0.

Fatigue Loading.—Periodic or non-periodic fluctuating loading applied to a test specimen or experiencedby a structure in service (also known as cyclic loading).

Fatigue Notch Factor*.—The fatigue notch factor, Kf (also called fatigue strength reduction factor), is theratio of the fatigue strength of a specimen with no stress concentration to the fatigue strength of a specimen

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with a stress concentration at the same number of cycles for the same conditions. NOTE—In specifying Kf,it is necessary to specify the geometry, mode of loading, and the values of Smax, Sm, and N for which it iscomputed.

Fatigue Notch Sensitivity.—The fatigue notch sensitivity, q, is a measure of the degree of agreementbetween Kf and Kt. NOTE—the definition of fatigue notch sensitivity is q = (Kf - 1)/(Kt - 1).

Heat.—All material identifiable to a single molten metal source. (All material from a heat is considered tohave the same composition. A heat may yield one or more ingots. A heat may be divided into several lotsby subsequent processing.)

Heat.—Heat is material which, in the case of batch melting, is cast at the same time from the same furnaceand is identified with the same heat number; or, in the case of continuous melting, is poured withoutinterruption. (See Table 9.2.4.2)

Heat.—Heat is a consolidated (vacuum hot pressed) billet having a distinct chemical composition. (SeeTable 9.2.4.2)

Hysteresis Diagram.—The stress-strain path during a fatigue cycle.

Isostrain Lines.—Lines representing constant levels of creep.

Isothermal Lines.—Lines of uniform temperature on a creep or stress-rupture curve.

Interrupted Test*.—Tests which have been stopped before failure because of some mechanical problem,e.g., power failure, load or temperature spikes.

Loading Amplitude.—The loading amplitude, Pa, Sa, or εa represents one-half of the range of a cycle. (Alsoknown as alternating load, alternating stress, or alternating strain.)

Loading Strain.—Loading strain is the change in strain during the time interval from the start of loadingto the instant of full-load application, sometimes called initial strain.

Loading (Unloading) Rate.—The time rate of change in the monotonically increasing (decreasing) portionof the load-time function.

Load Ratio.—The load ratio, R, A, or Rε, Aε, or Rσ, Aσ, is the algebraic ratio of the two loading parametersof a cycle; the two most widely used ratios are

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A-10

R 'minimum loadmaximum load

'Pmin

Pmax

Rσ 'Smin

Smax

Rε ' εmin/εmax

A 'loading amplitude

mean load'

Pa

Pm

orSa

SM

Aε 'strain amplitude

mean strain'

εa

εM

or εmax & εmin / εmax % εmin .

or

or

and

NOTE—load ratios R or Rε are generally used in MMPDS.

Longitudinal Direction.—Parallel to the principal direction of flow in a worked metal. For die forgings thisdirection is within ±15E of the predominate grain flow.

Long-Transverse Direction.—The transverse direction having the largest dimension, often called the“width” direction. For die forgings this direction is within ±15E of the longitudinal (predominate) graindirection and parallel, within ±15E, to the parting plane. (Both conditions must be met.)

Lot.—All material from a heat or single molten metal source of the same product type having the samethickness or configuration, and fabricated as a unit under the same conditions. If the material is heattreated, a lot is the above material processed through the required heat-treating operations as a unit.

Master Creep Equation.—An equation expressing combinations of stress, temperature, time and creep, ora set of equations expressing combinations of stress, temperature and time for given levels of creep.

Master Rupture Equation.—An equation expressing combinations of stress, temperature, and time thatcause complete separation (fracture or rupture) of the specimen.

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Pm 'Pmax % Pmin

2, or

Sm 'Smax % Smin

2, or

εm 'εmax % εmin

2,

Maximum Load.—The maximum load, Pmax, Smax, εmax is the load having the greatest algebraic value.

Mean Load.—The mean load, Pm, is the algebraic average of the maximum and minimum loads in constant-amplitude loading:

or the integral average of the instantaneous load values.

Median Fatigue Life.—The middlemost of the observed fatigue life values (arranged in order of magnitude)of the individual specimens in a group tested under identical conditions. In the case where an even numberof specimens are tested, it is the average of the two middlemost values (based on log lives in MMPDS).NOTE 1—The use of the sample median instead of the arithmetic mean (that is, the average) is usuallypreferred. NOTE 2—In the literature, the abbreviated term “fatigue life” usually has meant the medianfatigue life of the group. However, when applied to a collection of data without further qualification, theterm “fatigue life” is ambiguous.

Median Fatigue Strength at N Cycles.—An estimate of the stress level at which 50 percent of thepopulation would survive N cycles. NOTE—The estimate of the median fatigue strength is derived from aparticular point of the fatigue-life distribution, since there is no test procedure by which a frequencydistribution of fatigue strengths at N cycles can be directly observed. That is, one can not performconstant-life tests.

Melt.—Melt is a single homogeneous batch of molten metal for which all processing has been completedand the temperature has been adjusted and made ready to pour castings. (For metal-matrix composites, themolten metal includes unmelted reinforcements such as particles, fibers, or whiskers.) (See Table 9.1.6.2)

Minimum Load.—The minimum load, Pmin, Smin, or εmin, is the load having the least algebraic value.

Nominal Hole Diameters.—Nominal hole diameters for deformable shank fasteners shall be according toTable 9.4.1.2(a). When tests are made with hole diameters other than those tabulated, hole sizes used shallbe noted in the report and on the proposed joint allowables table.

Nominal Shank Diameter.—Nominal shank diameter of fasteners with shank diameters equal to those usedfor standard size bolts and screws (NAS 618 sizes) shall be the decimal equivalents of stated fractional ornumbered sizes. These diameters are those listed in the fourth column of Table 9.7.1.1. Nominal shankdiameters for nondeformable shank blind fasteners are listed in the fifth column of Table 9.7.1.1. Nominalshank diameters for other fasteners shall be the average of required maximum and minimum shankdiameters.

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Nondeformable Shank Fasteners.—A fastener whose shank does not deform in the grip area during normalinstallation processes.

Outlier*—An experimental observation which deviates markedly from other observations in the sample.An outlier is often either an extreme value of the variability in the data, or the result of gross deviation inthe material or experimental procedure.

Peak.—The point at which the first derivative of the load-time history changes from a positive to a negativesign; the point of maximum load in constant-amplitude loading.

Plane Strain.—The stress state in which all strains occur only in the principal loading plane. No strainsoccur out of the plane, i.e., εz = 0, and σz … 0.

Plane Stress.—The stress state in which all stresses occur only in the principal loading plane. No stressesoccur out of the plane, i.e., σz = 0, and εz … 0.

Plastic Strain During Loading.—Plastic strain during loading is the portion of the strain during loadingdetermined as the offset from the linear portion to the end of a stress-strain curve made during loadapplication.

Plane-Strain Fracture Toughness.—A generic term now generally adopted for the critical plane-strainstress intensity factor characteristic of plane-strain fracture, symbolically denoted KIc. This is because incurrent fracture testing practices, specification of the slowly increasing load test of specimen materials inthe plane-strain stress state and in opening mode (I) has been dominant.

Plane-Stress and Transitional Fracture Toughness.—A generic term denoting the critical stress intensityfactor associated with fracture behavior under nonplane-strain conditions. Because of plasticity effects andstable crack growth which can be encountered prior to fracture under these conditions, designation of aspecific value is dependent on the stage of crack growth detected during testing. Residual strength orapparent fracture toughness is a special case of plane-stress and transitional fracture toughness wherein thereference crack length is the initial pre-existing crack length and subsequent crack growth during the test isneglected.

Population.—All potential measurements having certain independent characteristics in common; i.e., “allpossible TUS(L) measurements for 17-7PH stainless steel sheet in TH1050 condition”.

Precision.*—The degree of mutual agreement among individual measurements. Relative to a method oftest, precision is the degree of mutual agreement among individual measurements made under prescribedlike conditions. The lack of precision in a measurement may be characterized as the standard deviation ofthe errors in measurement.

Primary Creep.—Creep occurring at a diminishing rate, sometimes called initial stage of creep.

Probability.—Ratio of possible number of favorable events to total possible number of equally likelyevents. For example, if a coin is tossed, the probability of heads is one-half (or 50 percent) because headscan occur one way and the total possible events are two, either heads or tails. Similarly, the probability of

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** Different from ASTM.

A-13

TUS 'TUS1 % TUS2 % ... % TUSn

n'

jn

i'1(TUSi)

n

throwing a three or greater on a die is 4/6 or 66.7 percent. Probability, as related to design allowables,means that chances of a material-property measurement equaling or exceeding a certain value (the one-sided lower tolerance limit) is 99 percent in the case of a A-basis value and 90 percent in the case of a B-basis value.

Range.—Range, ∆P, Sr, ∆ε, εr, ∆σ is the algebraic difference between successive valley and peak loads(positive range or increasing load range) or between successive peak and valley loads (negative range ordecreasing load range), see Figure 9.3.4.3. In constant-amplitude loading, for example, the range is given by∆P = Pmax - Pmin.

Rate of Creep.—The slope of the creep-time curve at a given time determined from a Cartesian plot.

Residual.*—The difference between the observed fatigue (log) life and the fatigue (log) life estimated fromthe fatigue model at a particular stress/strain level.

Runout.*—A test that has been terminated prior to failure. Runout tests are usually stopped at an arbitrarylife value because of time and economic considerations. NOTE—Runout tests are useful for estimating apseudo-fatigue-limit for a fatigue data sample.

Sample.—A finite number of observations drawn from the population.

Sample.—The number of specimens selected from a population for test purposes. NOTE—The method ofselecting the sample determines the population about which statistical inferences or generalization can bemade.

Sample Average (Arithmetic Mean).—The sum of all the observed values in a sample divided by thesample size (number). It is a point estimate of the population mean.

Sample Mean.—Average of all observed values in the sample. It is an estimate of population mean. Amean is indicated by a bar over the symbol for the value observed. Thus, the mean of n observations ofTUS would be expressed as:

Sample Median.—Value of the middle-most observation. If the sample is nearly normally distributed, thesample median is also an estimate of the population mean.

Sample Median.—The middle value when all observed values in a sample are arranged in order ofmagnitude if an odd number of samples are tested. If the sample size is even, it is the average of the twomiddlemost values. It is a point estimate of the population median, or 50 percentile point.

Sample Point Deviation.—The difference between an observed value and the sample mean.

Sample Standard Deviation.**—The standard deviation of the sample, s, is the square root of the samplevariance. It is a point estimate of the standard deviation of a population, a measure of the "spread" of the

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MMPDS31 January 2003

* This is appropriate, since a confidence level of 1 - α = 0.95 is used in establishing A and B-values.

** Different from ASTM.

A-14

S 2TUS '

jn

i'1TUSi & TUS 2

n & 1'

njn

i'1(TUSi)

2 & jn

i'1TUSi

2

n(n & 1)

frequency distribution of a population. NOTE—This value of s provides a statistic that is used incomputing interval estimates and several test statistics.

Sample Variance.*—Sample variance, s2, is the sum of the squares of the differences between eachobserved value and the sample average divided by the sample size minus one. It is a point estimate of thepopulation variance. NOTE—This value of s2 provides both an unbiased point estimate of the populationvariance and a statistic that is used on computing the interval estimates and several test statistics. Sometexts define s2 as “the sum of the squared differences between each observed value and the sample averagedivided by the sample size”, however, this statistic underestimates the population variance, particularly forsmall sample sizes.

Sample Variance.—The sum of the squared deviations, divided by n - 1, and, based on n observations ofTUS, expressed as

S-Basis.—The S-value is the minimum property value specified by the governing industry specification (asissued by standardization groups such as SAE Aerospace Materials Division, ASTM, etc.) or federal or mil-itary standards for the material. (See MIL-STD-970 for order of preference for specifications.) For certainproducts heat treated by the user (for example, steels hardened and tempered to a designated Ftu), the S-value may reflect a specified quality-control requirement. Statistical assurance associated with this value isnot known.

Secondary Creep.—Creep occurring at a constant rate, sometimes called second stage creep.

Short-Transverse Direction.—The transverse direction having the smallest dimension, often called the“thickness” direction. For die forgings this direction is within ±15E of the longitudinal (predominate) graindirection and perpendicular, within ±15E, to the parting plane. (Both conditions must be met.) Whenpossible, short transverse specimens shall be taken across the parting plane.

Significance Level (As Used Here).—Risk of concluding that two samples were drawn from differentpopulations when, in fact, they were drawn from the same population. A significance level of α = 0.05 isemployed through these Guidelines.*

Significance Level.—The stated probability (risk) that a given test of significance will reject the hypothesisthat a specified effect is absent when the hypothesis is true.

Significant (Statistically Significant).—An effect or difference between populations is said to be present ifthe value of a test statistic is significant, that is, lies outside of predetermined limits. NOTE—An effect thatis statistically significant may not have engineering importance.

S/N Curve for 50 Percent Survival.**—A curve fitted to the median values of fatigue life at each of severalstress levels. It is an estimate of the relationship between applied stress and the number of cycles-to-failurethat 50 percent of the population would survive. NOTE 1—This is a special case of the more general

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MMPDS31 January 2003

A-15

STUS'

jn

i'1TUSi & TUS 2

n & 1'

njn

i'1TUSi

2 & jn

i'1TUSi

2

n(n & 1)

K ' f a Y, ksi & in.1/2

definition of S/N curve for P percent survival. NOTE 2—In the literature, the abbreviated term “S/NCurve” usually has meant either the S/N curve drawn through the mean (averages) or through the medians(50 percent values) for the fatigue life values. Since the term “S/N Curve” is ambiguous, it should be usedonly when described appropriately. NOTE 3—Mean S/N curves (based on log lives) are shown inMMPDS.

S/N Diagram.—A plot of stress against the number of cycles to failure. The stress can be Smax, Smin, or Sa.The diagram indicates the S/N relationship for a specified value of Sm, A, or R and a specified probability ofsurvival. Typically, for N, a log scale (base 10) is used. Generally, for S, a linear scale is used, but a logscale is used occasionally. NOTE—Smax-versus-log N diagrams are used commonly in MMPDS.

Standard Deviation.—An estimate of the population standard deviation; the square root of the variance, or

Stress Intensity Factor.—A physical quantity describing the severity of a flaw in the stress field of a loadedstructural element. The gross stress in the material and flaw size are characterized parametrically by thestress intensity factor,

Stress-Rupture Test—A stress-rupture test is one in which time for rupture is measured, no deformationmeasurement being made during the test.

Tertiary Creep.—Creep occurring at an accelerating rate, sometimes called third stage creep.

Theoretical Stress Concentration Factor (or Stress Concentration Factor).—This factor, Kt, is the ratio ofthe nominal stress to the greatest stress in the region of a notch (or other stress concentrator) as determinedby the theory of elasticity (or by experimental procedures that give equivalent values). NOTE—The theoryof plasticity should not be used to determine Kt.

Tolerance Interval.—An interval computed so that it will include at least a stated percentage of thepopulation with a stated probability.

Tolerance Level.—The stated probability that the tolerance interval includes at least the stated percentage ofthe population. It is not the same as a confidence level, but the term confidence level is frequentlyassociated with tolerance intervals.

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MMPDS31 January 2003

* Different from ASTM.

A-16

Tolerance Limits.—The two statistics that define a tolerance interval. (One value may be “minus infinity”or “plus infinity”.)

Total Plastic Strain.—Total plastic strain at a specified time is equal to the sum of plastic strain duringloading plus creep.

Total Strain.—Total strain at any given time, including initial loading strain (which may include plasticstrain in addition to elastic strain) and creep strain, but not including thermal expansion.

Transition Fatigue Life.*—The point on a strain-life diagram where the elastic and plastic strains are equal.

Transverse Direction.—Perpendicular to the principal direction of flow in a worked metal; may be definedas T, LT or ST.

Typical Basis.—A typical property value is an average value and has no statistical assurance associated withit.

Waveform.—The shape of the peak-to-peak variation of a controlled mechanical test variable (for example,load, strain, displacement) as a function of time.

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MMPDS31 January 2003

A-17

ksi in. Megapascal meter(MPa @ m ½ )d

A.4 Conversion of U.S. Units of Measure Used in MMPDS to SI Units

Quantity orProperty

To Convert FromU. S. Unit

Multiplybya SI Unitb

Area in.2 645.16c Millimeter2 (mm2)

Force lb 4.4482 Newton (N)

Length in. 25.4c Millimeter (mm)

Stress ksi 6.895 Megapascal (MPa)d

Stress intensity factor 1.0989

Modulus 103 ksi 6.895 Gigapascal (GPa)d

Temperature EF F + 459.671.8

Kelvin (K)

Density (ω) lb/in.3 27.680 Megagram/meter3 (Mg/m3)

Specific heat (C) Btu/lb@F(or Btu@lb-1@F-1)

4.1868c Joule/(gram@Kelvin) (J/g@K) or (J@g-1 @K-1)

Thermalconductivity (K)

Btu/[(hr)(ft2)(F)/ft](or Btu@hr-1@ft-2@F-1@ft)

1.7307 Watt/(meter@Kelvin) W/(m@K) or (W@m-1@K-1)

Thermal expansion (α)

in./in./F(or [email protected]@F-1)

1.8 Meter/meter/Kelvin m/(m@K) or (m@m-1@K-1)

a Conversion factors to give significant figures are as specified in ASTM E 380, NASA SP-7012, second revision. NBS SpecialPublication 330, and Metals Engineering Quarterly. Note: Multiple conversions between U.S. and SI units should be avoidedbecause significant round-off errors may result.

b Prefix Multiple Prefix Multiplegiga (G) 109 milli (m) 10-3

mega (M) 106 micro (µ) 10-6

kilo (k) 103

c Conversion factor is exact.d One Pascal (Pa) = one Newton/meter2.

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MMPDS31 January 2003

A-18

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MMPDS-0131 January 2003

B-1Key: Underline indicates inactive for new design.

APPENDIX B

B.0 Alloy Index

Alloy Name Form Specification Section

250 Bar AMS 6512 2.5.1250 Sheet and Plate AMS 6520 2.5.1280 Sheet and Plate AMS 6521 2.5.1280 Bar AMS 6514 2.5.1354.0 Casting AMS-A-21180 3.9.1355.0 Permanent Mold Casting AMS 4281 3.9.2356.0 Sand Casting AMS 4217 3.9.4356.0 Investment Casting AMS 4260 3.9.4356.0 Permanent Mold Casting AMS 4284 3.9.4359.0 Casting AMS-A-21180 3.9.82014 Bare Sheet and Plate AMS 4028 3.2.12014 Bare Sheet and Plate AMS 4029 3.2.12014 Bar and Rod, Rolled or Cold Finished AMS 4121 3.2.12014 Forging AMS 4133 3.2.12014 Extrusion AMS 4153 3.2.12014 Forging AMS-A-22771 3.2.12014 Extruded Bar, Rod and Shapes AMS-QQ-A-200/2 3.2.12014 Rolled or Drawn Bar, Rod and Shapes AMS-QQ-A-225/4 3.2.12014 Clad Sheet and Plate AMS-QQ-A-250/3 3.2.12014 Forging AMS-QQ-A-367 3.2.12017 Bar and Rod, Rolled or Cold-Finished AMS 4118 3.2.22017 Rolled Bar and Rod AMS-QQ-A-225/5 3.2.22024 Bare Sheet and Plate AMS 4035 3.2.32024 Bare Sheet and Plate AMS 4037 3.2.32024 Tubing, Hydraulic, Seamless, Drawn AMS 4086 3.2.32024 Bar and Rod, Rolled or Cold-Finished AMS 4120 3.2.32024 Extrusion AMS 4152 3.2.32024 Extrusion AMS 4164 3.2.32024 Extrusion AMS 4165 3.2.32024 Extruded Bar, Rod and Shapes AMS-QQ-A-200/3 3.2.32024 Rolled or Drawn Bar, Rod and Wire AMS-QQ-A-225/6 3.2.32024 Bare Sheet and Plate AMS-QQ-A-250/4 3.2.32024 Clad Sheet and Plate AMS-QQ-A-250/5 3.2.32024 Tubing AMS-WW-T-700/3 3.2.32025 Die Forging AMS 4130 3.2.42026 Extruded Bars, Rods, and Profiles AMS 4338 3.2.52090 Sheet AMS 4251 3.2.62124 Plate AMS 4101 3.2.72124 Plate AMS-QQ-A-250/29 3.2.72219 Sheet and Plate AMS 4031 3.2.82219 Hand Forging AMS 4144 3.2.82219 Extrusion AMS 4162 3.2.82219 Extrusion AMS 4163 3.2.82219 Sheet and Plate AMS-QQ-A-250/30 3.2.82297 Plate AMS 4330 3.2.9

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MMPDS-0131 January 2003

Alloy Name Form Specification Section

B-2Key: Underline indicates inactive for new design.

2424 Sheet (Clad) AMS 4270 3.2.102424 Sheet (Bare) AMS 4273 3.2.102519 Plate MIL-DTL-46192 3.2.112524 Sheet and Plate AMS 4296 3.2.122618 Die and Hand Forgings AMS 4132 3.2.132618 Die Forging AMS-A-22771 3.2.132618 Forging AMS-QQ-A-367 3.2.134130 Bar and Forging AMS 6348 2.3.14130 Sheet, Strip and Plate AMS 6350 2.3.14130 Sheet, Strip and Plate AMS 6351 2.3.14130 Tubing AMS 6361 2.3.14130 Tubing AMS 6362 2.3.14130 Bar and Forging AMS 6370 2.3.14130 Tubing AMS 6371 2.3.14130 Tubing AMS 6373 2.3.14130 Tubing AMS 6374 2.3.14130 Bar and Forging AMS 6528 2.3.14130 Sheet, Strip and Plate AMS-S-18729 2.3.14130 Bar and Forging AMS-S-6758 2.3.14130 Tubing AMS-T-6736 2.3.14135 Sheet, Strip and Plate AMS 6352 2.3.14135 Tubing AMS 6365 2.3.14135 Tubing AMS 6372 2.3.14135 Tubing AMS-T-6735 2.3.14140 Bar and Forging AMS 6349 2.3.14140 Tubing AMS 6381 2.3.14140 Bar and Forging AMS 6382 2.3.14140 Sheet, Strip and Plate AMS 6395 2.3.14140 Bar and Forging AMS 6529 2.3.14140 Bar and Forging AMS-S-5626 2.3.14340 Sheet, Strip and Plate AMS 6359 2.3.14340 Bar and Forging AMS 6414 2.3.14340 Tubing AMS 6414 2.3.14340 Bar and Forging AMS 6415 2.3.14340 Tubing AMS 6415 2.3.14340 Sheet, Strip and Plate AMS 6454 2.3.14340 Bar and Forging AMS-S-5000 2.3.15052 Sheet and Plate AMS 4015 3.5.15052 Sheet and Plate AMS 4016 3.5.15052 Sheet and Plate AMS 4017 3.5.15052 Sheet and Plate AMS-QQ-A-250/8 3.5.15083 Bare Sheet and Plate AMS 4056 3.5.25083 Extruded Bar, Rod and Shapes AMS-QQ-A-200/4 3.5.25083 Bare Sheet and Plate AMS-QQ-A-250/6 3.5.25086 Extruded Bar, Rod and Shapes AMS-QQ-A-200/5 3.5.35086 Sheet and Plate AMS-QQ-A-250/7 3.5.35454 Extruded Bar, Rod and Shapes AMS-QQ-A-200/6 3.5.45454 Sheet and Plate AMS-QQ-A-250/10 3.5.45456 Extruded Bar, Rod and Shapes AMS-QQ-A-200/7 3.5.55456 Sheet and Plate AMS-QQ-A-250/9 3.5.56013 Sheet (T4) AMS 4347 3.6.16013 Sheet (T6) AMS 4216 3.6.16061 Sheet and Plate AMS 4025 3.6.26061 Sheet and Plate AMS 4026 3.6.2

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MMPDS-0131 January 2003

Alloy Name Form Specification Section

B-3Key: Underline indicates inactive for new design.

6061 Sheet and Plate AMS 4027 3.6.26061 Tubing Seamless, Drawn AMS 4080 3.6.26061 Tubing Seamless, Drawn AMS 4082 3.6.26061 Bar and Rod, Rolled or Cold Finished AMS 4115 3.6.26061 Bar and Rod, Cold Finished AMS 4116 3.6.26061 Bar and Rod, Rolled or Cold Finished AMS 4117 3.6.26061 Forging AMS 4127 3.6.26061 Extrusion AMS 4160 3.6.26061 Extrusion AMS 4161 3.6.26061 Extrusion AMS 4172 3.6.26061 Hand Forging AMS 4248 3.6.26061 Forging AMS-A-22771 3.6.26061 Extruded Rod, Bar Shapes and Tubing AMS-QQ-A-200/8 3.6.26061 Rolled Bar, Rod and Shapes AMS-QQ-A-225/8 3.6.26061 Extruded Rod, Bars and Shapes AMS 4150 3.6.26061 Extruded Rod, Bars and Shapes AMS 4173 3.6.26061 Sheet and Plate AMS-QQ-A-250/11 3.6.26061 Forging AMS-QQ-A-367 3.6.26061 Tubing Seamless, Drawn AMS-WW-T-700/6 3.6.26151 Die Forging AMS 4125 3.6.36151 Forging AMS-A-22771 3.6.37010 Plate AMS 4204 3.7.17010 Plate AMS 4205 3.7.17040 Plate AMS 4211 3.7.27049 Forging AMS-QQ-A-367 3.7.37049 Forging AMS 4111 3.7.37049 Extrusion AMS 4157 3.7.37049 Forging AMS-A-2271 3.7.37049 Plate AMS 4200 3.7.37050 Bare Plate AMS 4050 3.7.47050 Die Forging AMS 4107 3.7.47050 Hand Forging AMS 4108 3.7.47050 Bare Plate AMS 4201 3.7.47050 Die Forging AMS 4333 3.7.47050 Extruded Shape AMS 4340 3.7.47050 Extruded Shape AMS 4341 3.7.47050 Extruded Shape AMS 4342 3.7.47050 Forging AMS-A-22771 3.7.47055 Plate AMS 4206 3.7.57055 Extrusion AMS 4337 3.7.57055 Extrusion AMS 4324 3.7.57055 Extrusion AMS 4336 3.7.57075 Bare Sheet and Plate AMS 4044 3.7.67075 Bare Sheet and Plate AMS 4045 3.7.67075 Clad Sheet and Plate AMS 4049 3.7.67075 Bare Plate AMS 4078 3.7.67075 Bar and Rod, Rolled or Cold Finished AMS 4122 3.7.67075 Bar and Rod, Rolled or Cold Finished AMS 4123 3.7.67075 Bar and Rod, Rolled or Cold Finished AMS 4124 3.7.67075 Forging AMS 4126 3.7.67075 Die Forging AMS 4141 3.7.67075 Forging AMS 4147 3.7.67075 Bar and Rod, Rolled or Cold Finished AMS 4186 3.7.67075 Bar and Rod, Rolled or Cold Finished AMS 4187 3.7.6

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MMPDS-0131 January 2003

Alloy Name Form Specification Section

B-4Key: Underline indicates inactive for new design.

7075 Forging AMS-A-22771 3.7.67075 Extruded Bar, Rod and Shapes AMS-QQ-A-200/11, 15 3.7.67075 Rolled or Drawn Bar and Rod AMS-QQ-A-225/9 3.7.67075 Bare Sheet and Plate AMS-QQ-A-250/12, 24 3.7.67075 Clad Sheet and Plate AMS-QQ-A-250/13, 25 3.7.67075 Forging AMS-QQ-A-367 3.7.67149 Forging AMS 4320 3.7.37149 Forging AMS-A-2271 3.7.37149 Extrusion ASM 4343 3.7.37150 Bare Plate AMS 4252 (T7751) 3.7.77150 Bare Plate AMS 4306 (T6151) 3.7.77150 Extrusion AMS 4307 (T61511) 3.7.77150 Extrusion AMS 4345 (T77511) 3.7.77175 Die Forging AMS 4148 (T66) 3.7.87175 Die and Hand Forging AMS 4149 (T74) 3.7.87175 Hand Forging AMS 4179 (T7452) 3.7.87175 Extrusion AMS 4344 (T73511) 3.7.87175 Forging AMS-A-22771 3.7.87249 Hand Forging AMS 4334 3.7.97475 Bare Sheet AMS 4084 (T61) 3.7.107475 Bare Sheet AMS 4085 (T761) 3.7.107475 Bare Plate AMS 4089 (T7651) 3.7.107475 Bare Plate AMS 4090 (T651) 3.7.107475 Clad Sheet AMS 4100 (T761) 3.7.107475 Bare Plate AMS 4202 (T7351) 3.7.107475 Clad Sheet AMS 4207 (T61) 3.7.108630 Bar and Forging AMS 6280 2.3.18630 Tubing AMS 6281 2.3.18630 Sheet, Strip and Plate AMS-S-18728 2.3.18630 Bar and Forging AMS-S-6050 2.3.18630 Sheet, Strip and Plate AMS 6350 2.3.18735 Tubing AMS 6282 2.3.18735 Bar and Forging AMS 6320 2.3.18735 Sheet, Strip and Plate AMS 6357 2.3.18740 Bar and Forging AMS 6322 2.3.18740 Tubing AMS 6323 2.3.18740 Bar and Forging AMS 6327 2.3.18740 Sheet, Strip and Plate AMS 6358 2.3.18740 Bar and Forging AMS-S-6049 2.3.115-5PH Investment Casting AMS 5400 2.6.715-5PH Bar, Forging, Ring and Extrusion (CEVM) AMS 5659 2.6.715-5PH Sheet, Strip and Plate (CEVM) AMS 5862 2.6.717-4PH Investment Casting (H1100) AMS 5342 2.6.917-4PH Investment Casting (H1000) AMS 5343 2.6.917-4PH Investment Casting (H900) AMS 5344 2.6.917-4PH Sheet, Strip and Plate AMS 5604 2.6.917-4PH Bar, Forging and Ring AMS 5643 2.6.917-7PH Plate, Sheet and Strip AMS 5528 2.6.102024-T3 ARAMID Fiber Reinforced Sheet Laminate AMS 4254 7.5.1280 (300) Bar AMS 6514 2.5.1280 (300) Sheet and Plate AMS 6521 2.5.1300M (0.42C) Bar and Forging AMS 6257 2.3.1300M (0.42C) Tubing AMS 6257 2.3.1300M (0.42C) Bar and Forging AMS 6419 2.3.1

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MMPDS-0131 January 2003

Alloy Name Form Specification Section

B-5Key: Underline indicates inactive for new design.

300M (0.42C) Tubing AMS 6419 2.3.1300M (0.4C) Bar and Forging AMS 6417 2.3.1300M (0.4C) Tubing AMS 6417 2.3.14130 - N Tubing AMS 6360 2.3.14330V Bar and Forging AMS 6411 2.3.14330V Tubing AMS 6411 2.3.14330V Bar and Forging AMS 6427 2.3.14330V Tubing AMS 6427 2.3.14335V Bar and Forging AMS 6429 2.3.14335V Tubing AMS 6429 2.3.14335V Bar and Forging AMS 6430 2.3.14335V Tubing AMS 6430 2.3.14335V Sheet, Strip and Plate AMS 6433 2.3.14335V Sheet, Strip and Plate AMS 6435 2.3.15Cr-Mo-V Sheet, Strip and Plate AMS 6437 2.4.15Cr-Mo-V Bar and Forging (CEVM) AMS 6487 2.4.15Cr-Mo-V Bar and Forging AMS 6488 2.4.17475-T761 ARAMID Fiber Reinforced Sheet Laminate AMS 4302 7.5.29Ni-4Co-0.20C Sheet, Strip and Plate AMS 6523 2.4.29Ni-4Co-0.20C Sheet, Strip and Plate AMS 6524 2.4.39Ni-4Co-0.20C Bar and Forging, Tubing AMS 6526 2.4.3A201.0 Casting (T7 Temper) AMS-A-21180 3.8.1A-286 Sheet, Strip and Plate AMS 5525 6.2.1A-286 Bar, Forging, Tubing and Ring AMS 5731 6.2.1A-286 Bar, Forging, Tubing and Ring AMS 5732 6.2.1A-286 Bar, Forging and Tubing AMS 5734 6.2.1A-286 Bar, Forging and Tubing AMS 5737 6.2.1A356.0 Casting AMS 4218 3.9.5A356.0 Casting AMS-A-21180 3.9.5A357.0 Casting AMS-A-21180 3.9.6AerMet 100 Bar and Forging AMS 6478 2.5.3AerMet 100 Bar and Forging AMS 6532 2.5.3AF1410 Bar and Forging AMS 6527 2.5.2AISI 1025 Sheet, Strip, and Plate AMS 5046 2.2.1AISI 1025 Bar ASTM A 108 2.2.1AISI 1025 Sheet and Strip AMS-S-7952 2.2.1AISI 1025 Tubing AMS 5077 2.2.1AISI 1025 - N Seamless Tubing AMS 5075 2.2.1AISI 1025 - N Tubing AMS 5077 2.2.1AISI 1025 - N Tubing AMS-T-5066 2.2.1AISI 301 Sheet and Strip AMS 5517 2.7.1AISI 301 Sheet and Strip AMS 5518 2.7.1AISI 301 Sheet and Strip AMS 5519 2.7.1AISI 301 Sheet, Strip and Plate AMS 5901 2.7.1AISI 301 Sheet and Strip (175 ksi) AMS 5902 2.7.1AISI 302 Sheet, Strip and Plate AMS 5516 2.7.1AISI 302 Sheet and Strip (125 ksi) AMS 5903 2.7.1AISI 302 Sheet and Strip (150 ksi) AMS 5904 2.7.1AISI 302 Sheet and Strip (175 ksi) AMS 5905 2.7.1AISI 302 Sheet and Strip (185 ksi) AMS 5906 2.7.1AISI 304 Sheet and Strip AMS 5913 2.7.1AISI 304 Sheet, Strip and Plate (125 ksi) AMS 5910 2.7.1AISI 304 Sheet and Strip (150 ksi) AMS 5911 2.7.1AISI 304 Sheet and Strip (175 ksi) AMS 5912 2.7.1

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MMPDS-0131 January 2003

Alloy Name Form Specification Section

B-6Key: Underline indicates inactive for new design.

AISI 304 Sheet and Strip (185 ksi) AMS 5913 2.7.1AISI 316 Sheet and Strip AMS 5524 2.7.1AISI 316 Sheet, Strip and Plate (125 ksi) AMS 5907 2.7.1AM100A Investment Casting AMS 4455 4.3.1AM100A Permanent Mold Casting AMS 4483 4.3.1AM-350 Sheet and Strip AMS 5548 2.6.1AM-355 Sheet and Strip AMS 5547 2.6.2AM-355 Plate AMS 5549 2.6.2AM-355 Bar, Forging and Forging Stock AMS 5743 2.6.2AZ31B Sheet and Plate AMS 4375 4.2.1AZ31B Plate AMS 4376 4.2.1AZ31B Sheet and Plate AMS 4377 4.2.1AZ31B Forging ASTM B 91 4.2.1AZ31B Extrusion ASTM B 107 4.2.1AZ61A Extrusion AMS 4350 4.2.2AZ61A Forging ASTM B 91 4.2.2AZ91C/AZ91E Sand Casting AMS 4437 4.3.2AZ91C/AZ91E Sand Casting AMS 4446 4.3.2AZ91C/AZ91E Investment Casting AMS 4452 4.3.2AZ92A Sand Casting AMS 4434 4.3.3AZ92A Permanent Mold Casting AMS 4484 4.3.3AZ92A Investment Casting AMS 4453 4.3.3C355.0 Casting AMS-A-21180 3.9.3Copper Beryllium Strip (TB00) AMS 4530 7.3.2Copper Beryllium Strip (TD02) AMS 4532 7.3.2Copper Beryllium Bar and Rod (TF00) AMS 4533 7.3.2Copper Beryllium Bar and Rod (TH04) AMS 4534 7.3.2Copper Beryllium Mechanical tubing (TF00) AMS 4535 7.3.2Copper Beryllium Bar, Rod, Shapes and Forging (TB00) AMS 4650 7.3.2Copper Beryllium Bar and Rod (TD04) AMS 4651 7.3.2Copper Beryllium Sheet (TB00, TD01, TD02, TD04) ASTM B 194 7.3.2CP Titanium Sheet, Strip and Plate AMS 4900 5.2.1CP Titanium Sheet, Strip and Plate AMS 4901 5.2.1CP Titanium Sheet, Strip and Plate AMS 4902 5.2.1CP Titanium Bar AMS 4921 5.2.1CP Titanium Extruded Bars and Shapes AMS-T-81556 5.2.1CP Titanium Sheet, Strip and Plate AMS-T-9046 5.2.1CP Titanium Bar MIL-T-9047 5.2.1Custom 450 Bar, Forging, Tubing, Wire and Ring (air melted) AMS 5763 2.6.3Custom 450 Bar, Forging, Tubing, Wire and Ring (CEM) AMS 5773 2.6.3Custom 455 Tubing (welded) AMS 5578 2.6.4Custom 455 Bar and Forging AMS 5617 2.6.4Custom 465 Bars, Wires, and Forgings AMS 5936 2.6.5D357.0 Sand Composite Casting AMS 4241 3.9.7D6AC Bar and Forging AMS 6431 2.3.1D6AC Tubing AMS 6431 2.3.1D6AC Bar and Forging AMS 6439 2.3.1D6AC Sheet, Strip and Plate AMS 6439 2.3.1EZ33A Sand Casting AMS 4442 4.3.4Hastelloy X Sheet and Plate AMS 5536 6.3.1Hastelloy X Bar and Forging AMS 5754 6.3.1Haynes®230® Plate, Sheet, and Strip AMS 5878 6.3.9Haynes®230® Bar and Forging AMS 5891 6.3.9Haynes HR 120 Sheet, Strip and Plate AMS 5916 6.3.10

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MMPDS-0131 January 2003

Alloy Name Form Specification Section

B-7Key: Underline indicates inactive for new design.

HS 188 Sheet and Plate AMS 5608 6.4.2HS 188 Bar and Forging AMS 5772 6.4.2Hy-Tuf Bar and Forging AMS 6425 2.3.1Hy-Tuf Tubing AMS 6425 2.3.1Inconel 718 Investment Casting AMS 5383 6.3.5Inconel 718 Tubing; Creep Rupture AMS 5589 6.3.5Inconel 718 Tubing; Short-Time AMS 5590 6.3.5Inconel 718 Sheet, Strip and Plate; Creep Rupture AMS 5596 6.3.5Inconel 718 Sheet, Strip and Plate; Short-Time AMS 5597 6.3.5Inconel 718 Bar and Forging; Creep Rupture AMS 5662 6.3.5Inconel 718 Bar and Forging; Creep Rupture AMS 5663 6.3.5Inconel 718 Bar and Forging; Short-Time AMS 5664 6.3.5Inconel Alloy 600 Plate, Sheet and Strip AMS 5540 6.3.2Inconel Alloy 600 Tubing, Seamless AMS 5580 6.3.2Inconel Alloy 600 Bar and Rod ASTM B 166 6.3.2Inconel Alloy 600 Forging ASTM B 564 6.3.2Inconel Alloy 625 Sheet, Strip and Plate AMS 5599 6.3.3Inconel Alloy 625 Bar, Forging and Ring AMS 5666 6.3.3Inconel Alloy 706 Sheet, Strip and Plate AMS 5605 6.3.4Inconel Alloy 706 Sheet, Strip and Plate AMS 5606 6.3.4Inconel Alloy 706 Bar, Forging and Ring AMS 5701 6.3.4Inconel Alloy 706 Bar, Forging and Ring AMS 5702 6.3.4Inconel Alloy 706 Bar, Forging and Ring AMS 5703 6.3.4Inconel Alloy X-750 Sheet, Strip and Plate; Annealed AMS 5542 6.3.6Inconel Alloy X-750 Bar and Forging; Equalized AMS 5667 6.3.6L-605 Sheet AMS 5537 6.4.1L-605 Bar and Forging AMS 5759 6.4.1Manganese Bronzes Casting AMS 4860 7.3.1Manganese Bronzes Casting AMS 4862 7.3.1MP159 Alloy Bar (solution treated and cold drawn) AMS 5842 7.4.2MP159 Alloy Bar (solution treated, cold drawn and aged) AMS 5843 7.4.2MP35N Alloy Bar (solution treated and cold drawn) AMS 5844 7.4.1MP35N Alloy Bar (solution treated, cold drawn and aged) AMS 5845 7.4.1N-155 Sheet AMS 5532 6.2.2N-155 Tubing (welded) AMS 5585 6.2.2N-155 Bar and Forging AMS 5768 6.2.2N-155 Bar and Forging AMS 5769 6.2.2PH13-8Mo Bar, Forging Ring and Extrusion (VIM+CEVM) AMS 5629 2.6.5PH15-7Mo Plate, Sheet and Strip AMS 5520 2.6.7QE22A Magnesium Sand Casting AMS 4418 4.3.5René 41 Plate, Sheet and Strip AMS 5545 6.3.7René 41 Bar and Forging AMS 5713 6.3.7René 41 - STA Bar and Forging AMS 5712 6.3.7Standard Grade Beryllium Sheet and Plate AMS 7902 7.2.1Standard Grade Beryllium Bar, Rod, Tubing and Machined Shapes AMS 7906 7.2.1Ti-10V-2Fe-3Al (Ti-10-2-3) Forging AMS 4983 5.5.3Ti-10V-2Fe-3Al (Ti-10-2-3) Forging AMS 4984 5.5.3Ti-10V-2Fe-3Al (Ti-10-2-3) Forging AMS 4986 5.5.3Ti-13V-11Cr-3Al Sheet, Strip and Plate AMS-T-9046 5.5.1Ti-13V-11Cr-3Al Bar MIL-T-9047 5.5.1Ti-15V-3Cr-3Sn-3Al (Ti-15-3-3-3) Sheet and Strip AMS 4914 5.5.2Ti-4.5Al-3V-2Fe-2Mo Sheet AMS 4899 5.4.3Ti-4.5Al-3V-2Fe-2Mo Bars, Wires, forgings and Rings AMS 4964 5.4.3Ti-5Al-2.5Sn Sheet, Strip and Plate AMS 4910 5.3.1

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MMPDS-0131 January 2003

Alloy Name Form Specification Section

B-8Key: Underline indicates inactive for new design.

Ti-5Al-2.5Sn Bar AMS 4926 5.3.1Ti-5Al-2.5Sn Forging AMS 4966 5.3.1Ti-5Al-2.5Sn Extruded Bar and Shapes AMS-T-81556 5.3.1Ti-5Al-2.5Sn Sheet, Strip and Plate AMS-T-9046 5.3.1Ti-5Al-2.5Sn Bar MIL-T-9047 5.3.1Ti-6Al-2Sn-4Zr-2Mo Sheet, Strip and Plate AMS 4919 5.3.3Ti-6Al-2Sn-4Zr-2Mo Bar AMS 4975 5.3.3Ti-6Al-2Sn-4Zr-2Mo Forging AMS 4976 5.3.3Ti-6Al-2Sn-4Zr-2Mo Sheet and Strip AMS-T-9046 5.3.3Ti-6Al-4V Sheet, Strip and Plate AMS 4911 5.4.1Ti-6Al-4V Die Forging AMS 4920 5.4.1Ti-6Al-4V Bar and Die Forging AMS 4928 5.4.1Ti-6Al-4V Extrusion AMS 4934 5.4.1Ti-6Al-4V Extrusion AMS 4935 5.4.1Ti-6Al-4V Casting AMS 4962 5.4.1Ti-6Al-4V Bar AMS 4967 5.4.1Ti-6Al-4V Sheet, Strip and Plate AMS-T-9046 5.4.1Ti-6Al-4V Bar AMS 4965 5.4.1Ti-6Al-4V Bar MIL-T-9047 5.4.1Ti6Al-6V-2Sn Sheet, Strip and Plate AMS 4918 5.4.2Ti6Al-6V-2Sn Bar and Forging AMS 4971 5.4.2Ti6Al-6V-2Sn Bar and Forging AMS 4978 5.4.2Ti6Al-6V-2Sn Bar and Forging AMS 4979 5.4.2Ti6Al-6V-2Sn Extruded Bar and Shapes AMS-T-81556 5.4.2Ti6Al-6V-2Sn Sheet, Strip and Plate AMS-T-9046 5.4.2Ti-8Al-1Mo-1V Sheet, Strip and Plate AMS 4915 5.3.2Ti-8Al-1Mo-1V Sheet, Strip and Plate AMS 4916 5.3.2Ti-8Al-1Mo-1V Forging AMS 4973 5.3.2Ti-8Al-1Mo-1V Sheet, Strip and Plate AMS-T-9046 5.3.2Ti-8Al-1Mo-1V Bar MIL-T-9047 5.3.2Waspaloy Plate, Sheet and Strip AMS 5544 6.3.8Waspaloy Forging AMS 5704 6.3.8Waspaloy Bar, Forgings and Ring AMS 5706 6.3.8Waspaloy Bar, Forgings and Ring AMS 5707 6.3.8Waspaloy Bar, Forgings and Ring AMS 5708 6.3.8Waspaloy Bar, Forgings and Ring AMS 5709 6.3.8ZE41A Magnesium Sand Casting AMS 4439 4.3.6ZK60A-F Extrusion ASTM B 107 4.2.3ZK60A-T5 Extrusion AMS 4352 4.2.3ZK60A-T5 Die and Hand Forging AMS 4362 4.2.3

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MMPDS-0131 January 2003

C-1Key: Underline indicates inactive for new design.

APPENDIX C

C.0 Specification Index

Specification Alloy Name Form/Application Section

AMS 4015 5052 Sheet and Plate 3.5.1AMS 4016 5052 Sheet and Plate 3.5.1AMS 4017 5052 Sheet and Plate 3.5.1AMS 4025 6061 Sheet and Plate 3.6.2AMS 4026 6061 Sheet and Plate 3.6.2AMS 4027 6061 Sheet and Plate 3.6.2AMS 4028 2014 Bare Sheet and Plate 3.2.1AMS 4029 2014 Bare Sheet and Plate 3.2.1AMS 4031 2219 Sheet and Plate 3.2.8AMS 4035 2024 Bare Sheet and Plate 3.2.3AMS 4037 2024 Bare Sheet and Plate 3.2.3AMS 4044 7075 Bare Sheet and Plate 3.7.6AMS 4045 7075 Bare Sheet and Plate 3.7.6AMS 4049 7075 Clad Sheet and Plate 3.7.6AMS 4050 7050 Bare Plate 3.7.4AMS 4056 5083 Bare Sheet and Plate 3.5.2AMS 4078 7075 Bare Plate 3.7.6AMS 4080 6061 Tubing Seamless, Drawn 3.6.2AMS 4082 6061 Tubing Seamless, Drawn 3.6.2AMS 4084 (T61) 7475 Bare Sheet 3.7.10AMS 4085 (T761) 7475 Bare Sheet 3.7.10AMS 4086 2024 Tubing, Hydraulic, Seamless, Drawn 3.2.3AMS 4089 (T7651) 7475 Bare Plate 3.7.10AMS 4090 (T651) 7475 Bare Plate 3.7.10AMS 4100 (T761) 7475 Clad Sheet 3.7.10AMS 4101 2124 Plate 3.2.7AMS 4107 7050 Die Forging 3.7.4AMS 4108 7050 Hand Forging 3.7.4AMS 4111 7049 Forging 3.7.3AMS 4115 6061 Bar and Rod, Rolled or Cold Finished 3.6.2AMS 4116 6061 Bar and Rod, Cold Finished 3.6.2AMS 4117 6061 Bar and Rod, Rolled or Cold Finished 3.6.2AMS 4118 2017 Bar and Rod, Rolled or Cold-Finished 3.2.2AMS 4120 2024 Bar and Rod, Rolled or Cold-Finished 3.2.3AMS 4121 2014 Bar and Rod, Rolled or Cold Finished 3.2.1AMS 4122 7075 Bar and Rod, Rolled or Cold Finished 3.7.6AMS 4123 7075 Bar and Rod, Rolled or Cold Finished 3.7.6AMS 4124 7075 Bar and Rod, Rolled or Cold Finished 3.7.6AMS 4125 6151 Die Forging 3.6.3AMS 4126 7075 Forging 3.7.6AMS 4127 6061 Forging 3.6.2AMS 4130 2025 Die Forging 3.2.4AMS 4132 2618 Die and Hand Forgings 3.2.13AMS 4133 2014 Forging 3.2.1AMS 4141 7075 Die Forging 3.7.6

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MMPDS-0131 January 2003

Specification Alloy Name Form/Application Section

C-2Key: Underline indicates inactive for new design.

AMS 4144 2219 Hand Forging 3.2.8AMS 4147 7075 Forging 3.7.6AMS 4148 (T66) 7175 Die Forging 3.7.8AMS 4149 (T74) 7175 Die and Hand Forging 3.7.8AMS 4150 6061 Extruded Rod, Bars, and Shapes 3.6.2AMS 4152 2024 Extrusion 3.2.3AMS 4153 2014 Extrusion 3.2.1AMS 4157 7049 Extrusion 3.7.3AMS 4160 6061 Extrusion 3.6.2AMS 4161 6061 Extrusion 3.6.2AMS 4162 2219 Extrusion 3.2.8AMS 4163 2219 Extrusion 3.2.8AMS 4164 2024 Extrusion 3.2.3AMS 4165 2024 Extrusion 3.2.3AMS 4172 6061 Extrusion 3.6.2AMS 4173 6061 Extruded Rod, Bars, and Shapes 3.6.2AMS 4179 (T7452) 7175 Hand Forging 3.7.8AMS 4186 7075 Bar and Rod, Rolled or Cold Finished 3.7.6AMS 4187 7075 Bar and Rod, Rolled or Cold Finished 3.7.6AMS 4200 7049 Plate 3.7.3AMS 4201 7050 Bare Plate 3.7.4AMS 4202 (T7351) 7475 Bare Plate 3.7.10AMS 4204 7010 Plate 3.7.1AMS 4205 7010 Plate 3.7.1AMS 4206 7055 Plate 3.7.5AMS 4207 (T61) 7475 Clad Sheet 3.7.10AMS 4211 7040 Plate 3.7.2AMS 4216 6013 (T4) Sheet 3.6.1AMS 4217 356.0 Sand Casting 3.9.4AMS 4218 A356.0 Casting 3.9.5AMS 4241 D357.0 Sand Composite Casting 3.9.7AMS 4248 6061 Hand Forging 3.6.2AMS 4251 2090 Sheet 3.2.6AMS 4252 (T7751) 7150 Bare Plate 3.7.7AMS 4254 2024-T3 ARAMID Fiber Reinforced Sheet Laminate 7.5.1AMS 4260 356.0 Investment Casting 3.9.4AMS 4270 2424 (Clad) Sheet 3.2.10AMS 4273 2424 (Bare) Sheet 3.2.10AMS 4281 355.0 Permanent Mold Casting 3.9.2AMS 4284 356.0 Permanent Mold Casting 3.9.4AMS 4296 2524-T3 Sheet and Plate 3.2.12AMS 4302 7475-T761 ARAMID Fiber

ReinforcedSheet Laminate 7.5.2

AMS 4306 (T6151) 7150 Bare Plate 3.7.7AMS 4307 (T61511) 7150 Extrusion 3.7.7AMS 4320 7149 Forging 3.7.3AMS 4324 7055 Extrusion 3.7.5AMS 4330 2297 Plate 3.2.9AMS 4333 7050 Die Forging 3.7.4AMS 4334 7249 Hand Forging 3.7.9AMS 4336 7055 Extrusion 3.7.5AMS 4337 7055 Extrusion 3.7.5AMS 4338 2026 Bars, Rods, and Profiles 3.2.5AMS 4340 7050 Extruded Shape 3.7.4AMS 4341 7050 Extruded Shape 3.7.4AMS 4342 7050 Extruded Shape 3.7.4

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MMPDS-0131 January 2003

Specification Alloy Name Form/Application Section

C-3Key: Underline indicates inactive for new design.

AMS 4343 7149 Extrusion 3.7.3AMS 4344 (T73511) 7175 Extrusion 3.7.8AMS 4345 (T77511) 7150 Extrusion 3.7.7AMS 4347 6013 (T6) Sheet 3.6.1AMS 4350 AZ61A Extrusion 4.2.2AMS 4352 ZK60A-T5 Extrusion 4.2.3AMS 4362 ZK60A-T5 Die and Hand Forging 4.2.3AMS 4375 AZ31B Sheet and Plate 4.2.1AMS 4376 AZ31B Plate 4.2.1AMS 4377 AZ31B Sheet and Plate 4.2.1AMS 4418 QE22A Magnesium Sand Casting 4.3.5AMS 4434 AZ92A Sand Casting 4.3.3AMS 4437 AZ91C/AZ91E Sand Casting 4.3.2AMS 4439 ZE41A Magnesium Sand Casting 4.3.6AMS 4442 EZ33A Sand Casting 4.3.4AMS 4446 AZ91C/AZ91E Sand Casting 4.3.2AMS 4452 AZ91C/AZ91E Investment Casting 4.3.2AMS 4453 AZ92A Investment Casting 4.3.3AMS 4455 AM100A Investment Casting 4.3.1AMS 4483 AM100A Permanent Mold Casting 4.3.1AMS 4484 AZ92A Permanent Mold Casting 4.3.3AMS 4530 Copper Beryllium Strip (TB00) 7.3.2AMS 4532 Copper Beryllium Strip (TD02) 7.3.2AMS 4533 Copper Beryllium Bar and Rod (TF00) 7.3.2AMS 4534 Copper Beryllium Bar and Rod (TH04) 7.3.2AMS 4535 Copper Beryllium Mechanical tubing (TF00) 7.3.2AMS 4650 Copper Beryllium Bar, Rod, Shapes and Forging (TB00) 7.3.2AMS 4651 Copper Beryllium Bar and Rod (TD04) 7.3.2AMS 4860 Manganese Bronzes Casting 7.3.1AMS 4862 Manganese Bronzes Casting 7.3.1AMS 4899 Ti-4.5Al-3V-2Fe-2Mo Sheet 5.4.3AMS 4900 CP Titanium Sheet, Strip and Plate 5.2.1AMS 4901 CP Titanium Sheet, Strip and Plate 5.2.1AMS 4902 CP Titanium Sheet, Strip and Plate 5.2.1AMS 4910 Ti-5Al-2.5Sn Sheet, Strip and Plate 5.3.1AMS 4911 Ti-6Al-4V Sheet, Strip and Plate 5.4.1AMS 4914 Ti-15V-3Cr-3Sn-3Al (Ti-15-3)-3-3 Sheet and Strip 5.5.2AMS 4915 Ti-8Al-1Mo-1V Sheet, Strip and Plate 5.3.2AMS 4916 Ti-8Al-1Mo-1V Sheet, Strip and Plate 5.3.2AMS 4918 Ti6Al-6V-2Sn Sheet, Strip and Plate 5.4.2AMS 4919 Ti-6Al-2Sn-4Zr-2Mo Sheet, Strip and Plate 5.3.3AMS 4920 Ti-6Al-4V Die Forging 5.4.1AMS 4921 CP Titanium Bar 5.2.1AMS 4926 Ti-5Al-2.5Sn Bar 5.3.1AMS 4928 Ti-6Al-4V Bar and Die Forging 5.4.1AMS 4934 Ti-6Al-4V Extrusion 5.4.1AMS 4935 Ti-6Al-4V Extrusion 5.4.1AMS 4962 Ti-6Al-4V Casting 5.4.1AMS 4964 Ti-4.5Al-3V-2Fe-2Mo Bars, Wires, Forgings and Rings 5.4.3AMS 4965 Tii-6Al-4V Bar 5.4.1AMS 4966 Ti-5Al-2.5Sn Forging 5.3.1AMS 4967 Ti-6Al-4V Bar 5.4.1AMS 4971 Ti6Al-6V-2Sn Bar and Forging 5.4.2AMS 4973 Ti-8Al-1Mo-1V Forging 5.3.2AMS 4975 Ti-6Al-2Sn-4Zr-2Mo Bar 5.3.3AMS 4976 Ti-6Al-2Sn-4Zr-2Mo Forging 5.3.3

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MMPDS-0131 January 2003

Specification Alloy Name Form/Application Section

C-4Key: Underline indicates inactive for new design.

AMS 4978 Ti6Al-6V-2Sn Bar and Forging 5.4.2AMS 4979 Ti6Al-6V-2Sn Bar and Forging 5.4.2AMS 4983 Ti-10V-2Fe-3Al (Ti-10-2-3) Forging 5.5.3AMS 4984 Ti-10V-2Fe-3Al (Ti-10-2-3) Forging 5.5.3AMS 4986 Ti-10V-2Fe-3Al (Ti-10-2-3) Forging 5.5.3AMS 5046 AISI 1025 Sheet, Strip, and Plate 2.2.1AMS 5075 AISI 1025 - N Seamless Tubing 2.2.1AMS 5077 AISI 1025 - N Tubing 2.2.1AMS 5342 17-4PH Investment Casting (H1100) 2.6.9AMS 5343 17-4PH Investment Casting (H1000) 2.6.9AMS 5344 17-4PH Investment Casting (H900) 2.6.9AMS 5383 Inconel 718 Investment Casting 6.3.5AMS 5400 15-5PH Investment Casting 2.6.7AMS 5513 AISI 301 Sheet, Strip and Plate 2.7.1AMS 5516 AISI 302 Sheet, Strip and Plate 2.7.1AMS 5517 AISI 301 Sheet and Strip (125 ksi) 2.7.1AMS 5518 AISI 301 Sheet and Strip (150 ksi) 2.7.1AMS 5519 AISI 301 Sheet and Strip (185 ksi) 2.7.1AMS 5520 PH15-7Mo Plate, Sheet and Strip 2.6.8AMS 5524 AISI 316 Sheet, Strip and Plate 2.7.1AMS 5525 A-286 Sheet, Strip and Plate 6.2.1AMS 5528 17-7PH Plate, Sheet and Strip 2.6.10AMS 5532 N-155 Sheet 6.2.2AMS 5536 Hastelloy X Sheet and Plate 6.3.1AMS 5537 L-605 Sheet 6.4.1AMS 5540 Inconel Alloy 600 Plate, Sheet and Strip 6.3.2AMS 5542 Inconel Alloy X-750 Sheet, Strip and Plate; Annealed 6.3.6AMS 5544 Waspaloy Plate, Sheet and Strip 6.3.8AMS 5545 René 41 Plate, Sheet and Strip 6.3.7AMS 5547 AM-355 Sheet and Strip 2.6.2AMS 5548 AM-350 Sheet and Strip 2.6.1AMS 5549 AM-355 Plate 2.6.2AMS 5578 Custom 455 Tubing (welded) 2.6.4AMS 5580 Inconel Alloy 600 Tubing, Seamless 6.3.2AMS 5585 N-155 Tubing (welded) 6.2.2AMS 5589 Inconel 718 Tubing; Creep Rupture 6.3.5AMS 5590 Inconel 718 Tubing; Short-Time 6.3.5AMS 5596 Inconel 718 Sheet, Strip and Plate; Creep Rupture 6.3.5AMS 5597 Inconel 718 Sheet, Strip and Plate; Short-Time 6.3.5AMS 5599 Inconel Alloy 625 Sheet, Strip and Plate 6.3.3AMS 5604 17-4PH Sheet, Strip and Plate 2.6.9AMS 5605 Inconel Alloy 706 Sheet, Strip and Plate 6.3.4AMS 5606 Inconel Alloy 706 Sheet, Strip and Plate 6.3.4AMS 5608 HS 188 Sheet and Plate 6.4.2AMS 5617 Custom 455 Bar and Forging 2.6.4AMS 5629 PH13-8Mo Bar, Forging Ring and Extrusion (VIM+CEVM) 2.6.6AMS 5643 17-4PH Bar, Forging and Ring 2.6.9AMS 5659 15-5PH Bar, Forging, Ring and Extrusion (CEVM) 2.6.7AMS 5662 Inconel 718 Bar and Forging; Creep Rupture 6.3.5AMS 5663 Inconel 718 Bar and Forging; Creep Rupture 6.3.5AMS 5664 Inconel 718 Bar and Forging; Short-Time 6.3.5AMS 5666 Inconel Alloy 625 Bar, Forging and Ring 6.3.3AMS 5667 Inconel Alloy X-750 Bar and Forging; Equalized 6.3.6AMS 5701 Inconel Alloy 706 Bar, Forging and Ring 6.3.4AMS 5702 Inconel Alloy 706 Bar, Forging and Ring 6.3.4AMS 5703 Inconel Alloy 706 Bar, Forging and Ring 6.3.4

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MMPDS-0131 January 2003

Specification Alloy Name Form/Application Section

C-5Key: Underline indicates inactive for new design.

AMS 5704 Waspaloy Forging 6.3.8AMS 5706 Waspaloy Bar, Forgings and Ring 6.3.8AMS 5707 Waspaloy Bar, Forgings and Ring 6.3.8AMS 5708 Waspaloy Bar, Forgings and Ring 6.3.8AMS 5709 Waspaloy Bar, Forgings and Ring 6.3.8AMS 5712 René 41 - STA Bar and Forging 6.3.7AMS 5713 René 41 Bar and Forging 6.3.7AMS 5731 A-286 Bar, Forging, Tubing and Ring 6.2.1AMS 5732 A-286 Bar, Forging, Tubing and Ring 6.2.1AMS 5734 A-286 Bar, Forging and Tubing 6.2.1AMS 5737 A-286 Bar, Forging and Tubing 6.2.1AMS 5743 AM-355 Bar, Forging and Forging Stock 2.6.2AMS 5754 Hastelloy X Bar and Forging 6.3.1AMS 5759 L-605 Bar and Forging 6.4.1AMS 5763 Custom 450 Bar, Forging, Tubing, Wire and Ring (air melted) 2.6.3AMS 5768 N-155 Bar and Forging 6.2.2AMS 5769 N-155 Bar and Forging 6.2.2AMS 5772 HS 188 Bar and Forging 6.4.2AMS 5773 Custom 450 Bar, Forging, Tubing, Wire and Ring (CEM) 2.6.3AMS 5842 MP159 Alloy Bar (solution treated and cold drawn) 7.4.2AMS 5843 MP159 Alloy Bar (solution treated, cold drawn and aged) 7.4.2AMS 5844 MP35N Alloy Bar (solution treated and cold drawn) 7.4.1AMS 5845 MP35N Alloy Bar (solution treated, cold drawn and aged) 7.4.1AMS 5862 15-5PH Sheet, Strip and Plate (CEVM) 2.6.7AMS 5878 Haynes®230® Plate, Sheet and Strip 6.3.9AMS 5891 Haynes®230® Bar and Forging 6.3.9AMS 5901 AISI 301 Plate, Sheet and Strip 2.7.1AMS 5902 AISI 301 Sheet and Strip (175 ksi) 2.7.1AMS 5903 AISI 302 Sheet and Strip (125 ksi) 2.7.1AMS 5904 AISI 302 Sheet and Strip (150 ksi) 2.7.1AMS 5905 AISI 302 Sheet and Strip (175 ksi) 2.7.1AMS 5906 AISI 302 Sheet and Strip (185 ksi) 2.7.1AMS 5907 AISI 316 Sheet, Strip and Plate (125 ksi) 2.7.1AMS 5910 AISI 304 Sheet, Strip and Plate (125 ksi) 2.7.1AMS 5911 AISI 304 Sheet and Strip (150 ksi) 2.7.1AMS 5912 AISI 304 Sheet and Strip (175 ksi) 2.7.1AMS 5913 AISI 304 Sheet and Strip (185 ksi) 2.7.1AMS 5916 Haynes HR-120 Sheet, Strip and Plate 6.3.10AMS 5936 Cutsom 465 Bar, Wires and Forgings 2.6.5AMS 6257 300M (0.42C) Bar and Forging 2.3.1AMS 6257 300M (0.42C) Tubing 2.3.1AMS 6280 8630 Bar and Forging 2.3.1AMS 6281 8630 Tubing 2.3.1AMS 6282 8735 Tubing 2.3.1AMS 6320 8735 Bar and Forging 2.3.1AMS 6322 8740 Bar and Forging 2.3.1AMS 6323 8740 Tubing 2.3.1AMS 6327 8740 Bar and Forging 2.3.1AMS 6348 4130 Bar and Forging 2.3.1AMS 6349 4140 Bar and Forging 2.3.1AMS 6350 4130 Sheet, Strip and Plate 2.3.1AMS 6350 8630 Sheet, Strip and Plate 2.3.1AMS 6351 4130 Sheet, Strip and Plate 2.3.1AMS 6352 4135 Sheet, Strip and Plate 2.3.1AMS 6355 8630 Tubing 2.3.1AMS 6357 8735 Sheet, Strip and Plate 2.3.1

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MMPDS-0131 January 2003

Specification Alloy Name Form/Application Section

C-6Key: Underline indicates inactive for new design.

AMS 6358 8740 Sheet, Strip and Plate 2.3.1AMS 6359 4340 Sheet, Strip and Plate 2.3.1AMS 6360 4130 Tubing (normalized) 2.3.1AMS 6361 4130 Tubing 2.3.1AMS 6362 4130 Tubing 2.3.1AMS 6365 4135 Tubing 2.3.1AMS 6370 4130 Bar and Forging 2.3.1AMS 6371 4130 Tubing 2.3.1AMS 6372 4135 Tubing 2.3.1AMS 6373 4130 Tubing 2.3.1AMS 6374 4130 Tubing 2.3.1AMS 6381 4140 Tubing 2.3.1AMS 6382 4140 Bar and Forging 2.3.1AMS 6395 4140 Sheet, Strip and Plate 2.3.1AMS 6411 4330V Bar and Forging 2.3.1AMS 6411 4330V Tubing 2.3.1AMS 6414 4340 Bar and Forging 2.3.1AMS 6414 4340 Tubing 2.3.1AMS 6415 4340 Bar and Forging 2.3.1AMS 6415 4340 Tubing 2.3.1AMS 6417 300M (0.4C) Bar and Forging 2.3.1AMS 6417 300M (0.4C) Tubing 2.3.1AMS 6419 300M (0.42C) Bar and Forging 2.3.1AMS 6419 300M (0.42C) Tubing 2.3.1AMS 6425 Hy-Tuf Bar and Forging 2.3.1AMS 6425 Hy-Tuf Tubing 2.3.1AMS 6427 4330V Bar and Forging 2.3.1AMS 6427 4330V Tubing 2.3.1AMS 6429 4335V Bar and Forging 2.3.1AMS 6429 4335V Tubing 2.3.1AMS 6430 4335V Bar and Forging 2.3.1AMS 6430 4335V Tubing 2.3.1AMS 6431 D6AC Bar and Forging 2.3.1AMS 6431 D6AC Tubing 2.3.1AMS 6433 4335V Sheet, Strip and Plate 2.3.1AMS 6435 4335V Sheet, Strip and Plate 2.3.1AMS 6437 5Cr-Mo-V Sheet, Strip and Plate 2.4.1AMS 6439 D6AC Sheet, Strip and Plate 2.3.1AMS 6439 D6AC Bar and Forging 2.3.1AMS 6454 4340 Sheet, Strip and Plate 2.3.1AMS 6478 AerMet 100 Bar and Forging 2.5.3AMS 6487 5Cr-Mo-V Bar and Forging (CEVM) 2.4.1AMS 6488 5Cr-Mo-V Bar and Forging 2.4.1AMS 6512 250 Bar 2.5.1AMS 6514 280 (300) Bar 2.5.1AMS 6520 250 Sheet and Plate 2.5.1AMS 6521 280 (300) Sheet and Plate 2.5.1AMS 6523 9Ni-4Co-0.20C Sheet, Strip and Plate 2.4.2AMS 6524 9Ni-4Co-0.20C Sheet, Strip and Plate 2.4.3AMS 6526 9Ni-4Co-0.20C Bar and Forging, Tubing 2.4.3AMS 6527 AF1410 Bar and Forging 2.5.2AMS 6528 4130 Bar and Forging 2.3.1AMS 6529 4140 Bar and Forging 2.3.1AMS 6532 AerMet 100 Bar and Forging 2.5.3AMS 7902 Standard Grade Beryllium Sheet and Plate 7.2.1AMS 7906 Standard Grade Beryllium Bar, Rod, Tubing and Machined Shapes 7.2.1

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MMPDS-0131 January 2003

Specification Alloy Name Form/Application Section

C-7Key: Underline indicates inactive for new design.

AMS-A-21180 A201.0 Casting (T7 Temper) 3.8.1AMS-A-21180 354.0 Casting 3.9.1AMS-A-21180 C355.0 Casting 3.9.3AMS-A-21180 A356.0 Casting 3.9.5AMS-A-21180 A357.0 Casting 3.9.6AMS-A-21180 359.0 Casting 3.9.8AMS-A-22771 2014 Forging 3.2.1AMS-A-22771 2618 Die Forging 3.2.13AMS-A-22771 6061 Forging 3.6.2AMS-A-22771 6151 Forging 3.6.3AMS-A-22771 7049/7149 Forging 3.7.3AMS-A-22771 7050 Forging 3.7.4AMS-A-22771 7075 Forging 3.7.6AMS-A-22771 7175 Forging 3.7.8AMS-QQ-A-367 2014 Forging 3.2.1AMS-QQ-A-367 2618 Forging 3.2.13AMS-QQ-A-367 6061 Forging 3.6.2AMS-QQ-A-367 7049/7149 Forging 3.7.3AMS-QQ-A-367 7075 Forging 3.7.6AMS-QQ-A-200/2 2014 Extruded Bar, Rod and Shapes 3.2.1AMS-QQ-A-200/3 2024 Extruded Bar, Rod and Shapes 3.2.3AMS-QQ-A-200/4 5083 Extruded Bar, Rod and Shapes 3.5.2AMS-QQ-A-200/5 5086 Extruded Bar, Rod and Shapes 3.5.3AMS-QQ-A-200/6 5454 Extruded Bar, Rod and Shapes 3.5.4AMS-QQ-A-200/7 5456 Extruded Bar, Rod and Shapes 3.5.5AMS-QQ-A-200/8 6061 Extruded Rod, Bar Shapes and Tubing 3.6.2AMS-QQ-A-200/11, 15 7075 Extruded Bar, Rod and Shapes 3.7.6AMS-QQ-A-225/4 2014 Rolled or Drawn Bar, Rod and Shapes 3.2.1AMS-QQ-A-225/5 2017 Rolled Bar and Rod 3.2.2AMS-QQ-A-225/6 2024 Rolled or Drawn Bar, Rod and Wire 3.2.3AMS-QQ-A-225/8 6061 Rolled Bar, Rod and Shapes 3.6.2AMS-QQ-A-225/9 7075 Rolled or Drawn Bar and Rod 3.7.6AMS-QQ-A-250/3 2014 Clad Sheet and Plate 3.2.1AMS-QQ-A-250/4 2024 Bare Sheet and Plate 3.2.3AMS-QQ-A-250/5 2024 Clad Sheet and Plate 3.2.3AMS-QQ-A-250/6 5083 Bare Sheet and Plate 3.5.2AMS-QQ-A-250/7 5086 Sheet and Plate 3.5.3AMS-QQ-A-250/8 5052 Sheet and Plate 3.5.1AMS-QQ-A-250/9 5456 Sheet and Plate 3.5.5AMS-QQ-A-250/10 5454 Sheet and Plate 3.5.4AMS-QQ-A-250/11 6061 Sheet and Plate 3.6.2AMS-QQ-A-250/12, 24 7075 Bare Sheet and Plate 3.7.6AMS-QQ-A-250/13, 25 7075 Clad Sheet and Plate 3.7.6AMS-QQ-A-250/29 2124 Plate 3.2.7AMS-QQ-A-250/30 2219 Sheet and Plate 3.2.8AMS-QQ-A-367 7049 Forging 3.7.3AMS-S-5000 4340 Bar and Forging 2.3.1AMS-S-5626 4140 Bar and Forging 2.3.1AMS-S-6049 8740 Bar and Forging 2.3.1AMS-S-6050 8630 Bar and Forging 2.3.1AMS-S-6758 4130 Bar and Forging 2.3.1AMS-S-7952 AISI 1025 Sheet and Strip 2.2.1AMS-S-18728 8630 Sheet, Strip and Plate 2.3.1AMS-S-18729 4130 Sheet, Strip and Plate 2.3.1AMS-T-5066 AISI 1025 - N Tubing 2.2.1AMS-T-6735 4135 Tubing 2.3.1

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MMPDS-0131 January 2003

Specification Alloy Name Form/Application Section

C-8Key: Underline indicates inactive for new design.

AMS-T-6736 4130 Tubing 2.3.1AMS-T-81556 CP Titanium Extruded Bars and Shapes 5.2.1AMS-T-81556 Ti-5Al-2.5Sn Extruded Bar and Shapes 5.3.1AMS-T-81556 Ti6Al-6V-2Sn Extruded Bar and Shapes 5.4.2AMS-T-9046 CP Titanium Sheet, Strip and Plate 5.2.1AMS-T-9046 Ti-5Al-2.5Sn Sheet, Strip and Plate 5.3.1AMS-T-9046 Ti-8Al-1Mo-1V Sheet, Strip and Plate 5.3.2AMS-T-9046 Ti-6Al-2Sn-4Zr-2Mo Sheet and Strip 5.3.3AMS-T-9046 Ti-6Al-4V Sheet, Strip and Plate 5.4.1AMS-T-9046 Ti6Al-6V-2Sn Sheet, Strip and Plate 5.4.2AMS-T-9046 Ti-13V-11Cr-3Al Sheet, Strip and Plate 5.5.1AMS-WW-T-700/3 2024 Tubing 3.2.3AMS-WW-T-700/6 6061 Tubing Seamless, Drawn 3.6.2ASTM A 108 AISI 1025 Bar 2.2.1ASTM B 91 AZ31B Forging 4.2.1ASTM B 91 AZ61A Forging 4.2.2ASTM B 107 ZK60A-F Extrusion 4.2.3ASTM B 107 AZ31B Extrusion 4.2.1ASTM B 166 Inconel Alloy 600 Bar and Rod 6.3.2ASTM B 194 Copper Beryllium Sheet (TB00, TD01, TD02, TD04) 7.3.2ASTM B 564 Inconel Alloy 600 Forging 6.3.2MIL-DTL-46192 2519 Plate 3.2.11MIL-T-9047 CP Titanium Bar 5.2.1MIL-T-9047 Ti-5Al-2.5Sn Bar 5.3.1MIL-T-9047 Ti-8Al-1Mo-1V Bar 5.3.2MIL-T-9047 Ti-6Al-4V Bar 5.4.1MIL-T-9047 Ti-13V-11Cr-3Al Bar 5.5.1

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D-1

D.0 Subject Index

A-Basis, 1-5, 9-9, 9-25AMS Specifications, 9-11Anderson-Darling Test

k-Sample Test, 9-77Normality, 9-82Pearsonality, 9-85Weibullness, 9-89

Applicability of Procedures, 9-5Approval Procedures, 9-5ASTM

ASTM A 370, 9-13, 9-15ASTM B 557, 9-13, 9-15ASTM B 769, 1-12, 9-13, 9-15ASTM B 831, 1-12, 9-13, 9-16ASTM C 693, 9-12, 9-16, 9-184ASTM C 714, 9-13, 9-16, 9-184ASTM D 2766, 9-13, 9-16, 9-184ASTM E 8, 1-8, 1-21, 9-12, 9-13, 9-15, 9-38ASTM E 9, 1-11, 9-12, 9-15ASTM E 21, 9-13ASTM E 29, 9-10ASTM E 83, 9-12, 9-31ASTM E 111, 9-12, 9-31, 9-183ASTM E 132, 9-13, 9-16, 9-183ASTM E 139, 9-12, 9-22ASTM E 143, 9-12, 9-183ASTM E 228, 9-12, 9-16, 9-184ASTM E 238, 1-12, 9-12, 9-15, 9-16ASTM E 399, 1-21, 9-13, 9-18, 9-24, 9-133ASTM E 466, 9-12, 9-17ASTM E 561, 9-13ASTM E 606, 9-12, 9-17, 9-33, 9-41, 9-45,

9-110ASTM E 647, 9-12, 9-17ASTM E 739, 9-40ASTM G 34, 9-12ASTM G 47, 9-13

B-Basis, 1-7, 9-9, 9-25Beams, Properties of

Aluminum, 3-518Magnesium, 4-53Steel, 2-237Titanium, 5-144

Bearing Failure, 1-28Bearing Properties, 1-12, 9-7Bearing Test Procedures, 9-106, 9-109Bearings, 8-172

Bending Failure, 1-28Biaxial Properties, 1-17

Modulus of Elasticity, 1-18Ultimate Stress, 1-19Yield Stress, 1-18

Biaxial Stress-Strain Curves, 9-198Brittle Fracture, 1-20

Analysis, 1-20Cast, Definition of, 9-30Clad Aluminum Alloy Plate, 9-107Coefficient of Thermal Expansion, 9-16Columns, 1-30

Aluminum, 3-519Local Instability, 1-30Magnesium, 4-53Primary Instability, 1-30Stable Sections, 1-30Steel, 2-237Test Results, 1-30Yield Stress, 1-32

Combinability of Data, 9-77Anderson-Darling k-Sample Test, 9-77F-Test, 9-77, 9-79t-Test, 9-77, 9-80

Compressive Failure, 1-26Compressive Properties, 1-11, 9-7Computational Procedures, 9-60

Derived Properties, 9-106, 9-109Nonparametric, 9-103Normal Distribution, 9-82Pearson Distribution, 9-82, 9-100Population Specification, 9-60Unknown Distribution, 9-103Weibull Distribution, 9-82, 9-102

Confidence, 9-9, A-6Confidence Interval, A-6Confidence Level, A-6Confidence Limit, A-7Creep/Stress Rupture, 1-13, 9-22, 9-234

Data Analysis, 9-137Data Generation, 9-46, 9-135Data Requirements, 9-35Equations, 9-138, 9-140Example Problems, 9-235Presentation of Data, 9-235Terminology, 9-135, 9-140

Data Basis, 9-8

APPENDIX D

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MMPDS-0131 January 2003

D-2

Data Format, 9-50A- and B-basis, 9-52Derived Properties, 9-51Fasteners, 9-55Stress-Strain Curves, 9-55Other Property, 9-56

Data Generation, 9-24Creep/Stress Rupture, 9-46Fatigue, 9-40Fatigue Crack Growth, 9-130Fracture Toughness, 9-133Fusion-Welded Joints, 9-48Mechanically Fastened Joints, 9-142Mechanical Properties, 9-24, 9-30Stress-Strain, 9-184

Data PresentationCreep-Rupture, 9-234Elevated Temperature Curves, 9-202Fatigue, 9-212Fatigue Crack Growth, 1-26, 9-228Fracture Toughness, 9-230Fusion-Welded Joints, 9-244Mechanically Fastened Joints, 9-240Room-Temperature Design Values, 9-179,

9-184Typical (Full-Range) Stress-Strain, 9-194Typical Stress-Strain, 9-184

Data Requirements, 9-24, 9-26, 9-29Creep/Stress Rupture, 9-26, 9-35Derived Properties, 9-26, 9-30Directly Calculated, 9-9, 9-26Elevated Temperature Properties, 9-26, 9-32Experimental Design, 9-40Fatigue, 9-27, 9-32, 9-40Fatigue Crack Growth, 9-27, 9-35Fracture Toughness, 9-35Fusion-Welded Joints, 9-40Mechanically Fastened Joints, 9-36Mechanical Properties, 9-24, 9-25, 9-27Modulus, 9-26, 9-31New Materials, 9-7, 9-24Physical Properties, 9-26, 9-27Stress-Strain, 9-28, 9-31

Data Submission, 9-50Definition of Terms, 9-30

Creep/Stress Rupture, 9-135Fatigue, 9-110Fracture Toughness, 9-133Mechanically Fastened Joints, 9-142Mechanical Properties, 9-14Statistics, A-6

Degrees of Freedom, 9-81, A-8Density, 9-16

Derived Properties, 9-30Design Mechanical Properties, 9-60

By Regression, 9-63, 9-64Determining Form of Distribution, 9-82Determining Population, 9-60Direct Computation,

Non Parametric, 9-103Pearson, 9-100Weibull, 9- 102

Example Problems, 9-162, 9-175Presentation, 9-179

Dimensionally Discrepant Castings, 9-11Direct Computation of Allowables, 9-60, 9-94,

9-104, 9-162 Nonparametric Distribution, 9-103Pearson Distribution, 9-100Weibull Distribution, 9-102

Distribution, Form of, 9-82Documentation Requirements, 9-5Elastic Properties, 9-183Element Properties

Aluminum, 3-518Magnesium, 4-53Steel, 2-237Titanium, 5-144

Elevated Temperature Curves, 1-13, 9-68, 9-202Data Requirements, 9-32Presentation, 9-203Working Curves, 9-202

Environmental Effects, 1-21Elongation, 1-8, 9-204Examples of Computation Procedures

Complex Exposure, 9-210Creep/Stress Rupture, 9-235Design Allowables, 9-162Fatigue, 9-212, 9-219, 9-223F-Test, 9-79Linear Regression, 9-104Strain-Departure Method, 9-185t-Test, 9-80

F-Distribution Fractiles, 9-253, 9-254F-Test, 9-79Failure

General, 1-28Identification code, 9-57, 9-58Instability, 1-29Local, 1-30Material, 1-28Types, 1-28

Fasteners, 9-142Data Format, 9-55H-Type, 9-144S-Type, 9- 144

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D-3

Fatigue, 9-8, 9-17, 9-110Data Analysis, 9-114, 9-127Data Generation, 9-40, 9-113, 9-223Data Requirements, 9-17, 9-110, 9-223, 9-34Example Problems, 9-212, 9-223Life Models, 9-115, 9-125, 9-221, 9-226,

9-227Load Control, 9-219Outliers, 9-124, 9-221, 9-227Presentation of Data, 1-15, 9-223Properties, 1-14Run-outs, 9-128, 9-222, 9-228Strain Control, 9-223Terminology, 9-40Test Planning, 9-40Time Dependent Effects, 9-130

Fatigue Crack Growth, 1-24, 9-17, 9-130, 9-228Crack-Growth Analysis, 1-24Data Analysis, 9-134Data Generation, 9-133Data Requirements, 9-35, 9-131Presentation of Data, 1-26, 9-228

Forgings, Definition of Grain Directions in, 9-15Fracture Toughness, 1-19, 9-18, 9-230

Analysis, 1-20, 9-133Apparent Fracture Toughness, 1-23Brittle Fracture, 1-20Critical Plane-Strain, 1-21Data Analysis, 9-133Data Generation, 9-35Data Requirements, 9-35Definitions, 9-133Environmental, 1-21Middle Tension Panels, 1-23, 9-19, 9-35,

9-134Plane Stress, 1-22, 9-18, 9-133Plane Strain, 1-21, 9-18, 9-133Presentation of Data, 9-230Transitional Stress States, 1-22, 9-133

Full-Range Stress-Strain Curves, 9-194Fusion-Welded Joints, 9-23, 9-40, 9-158

Data Analysis, 9-161Data Generation, 9-48, 9-159, 9-160Data Requirements, 9-40, 9-160Presentation of Data, 9-244

Goodness-of-Fit Tests, 9-82Anderson-Darling, 9-82Normality, 9-82Pearsonality, 9-85Weibullness, 9-83

Grain Direction, Treatment of, 9-106Grouped Data Analysis, 9-77Heat Requirements, 9-7

Indirect Design Allowables, 9-7, 9-60, 9-106Without Regression, 9-108With Regression, 9-109

Instability, 1-29Bending, 1-29Combined Loadings, 1-29Compression, 1-29Local, 1-30Torsion, 1-29

International System of Units, 1-3k-Sample Anderson-Darling Test, 9-77Larson-Miller Analysis, 9-138Location of Test Specimens, 9-14Lot Requirements, 9-7Material Failures, 1-28

Bearing, 1-28Bending, 1-28Combined Stress, 1-28Compression, 1-28Shear, 1-28Stress Concentrations, 1-28Tension, 1-28

Material Specifications, 9-11Maximum Likelihood Estimation, 9-129Mean Stress/Strain Effects, Evaluation of, 9-117Mechanical Properties, 9-60

Computation of Design Allowables, 9-60Derived Properties, 9-30, 9-106, 9-109Example Problems, 9-162, 9-175Presentation, 9-179Terminology for, 9-14Test Matrix, 9-29

Mechanically Fastened Joints, 9-22, 9-142Data Analysis, 9-144, 9-146, 9-148, 9-158Data Requirements, 9-36Definitions, 9-143Presentation of Data, 9-240

Melt, Definition of, 9-30Metallurgical Instability, 1-17Modulus of Elasticity, 1-9, 9-16, 9-31, 9-183,

9-206Modulus of Rigidity, 1-12NASM-1312, 9-11, 9-12, 9-22, 9-23, 9-38,

9-144 Nomenclature, 1-3Nonparametric Data Analysis, 9-103Normal Curve Statistics, 9-256Normality, Assessment of, 9-82Outliers, Treatment of, 9-124, 9-221, 9-227Pearson Method, 9-100

Anderson-Darling, 9-85Backoff, 9-85Probability Plot, 9-86

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MMPDS-0131 January 2003

D-4

Physical Properties, 9-16, 9-207Poisson’s Ratio, 1-8, 9-16, 9-183Presentation of Data, 9-162, 9-212

Creep/Stress Rupture, 9-234Design Allowables, 9-179Effect of Temperature Curves, 9-246Fatigue, 9-212Fatigue Crack Growth, 9-228Fracture Toughness, 9-230Fusion-Welded Joints, 9-244, 9-245Mechanically Fastened Joints, 9-240Physical Properties, 9-183Stress-Strain, 9-184

Primary Test Direction, 9-15Probability, A-12Probability Plots

Normal, 9-83Pearson, 9-86Weibull, 9-92

Proportional LimitShear, 1-12Stress, 9-201Tension and Compression 9-201

Pulleys, 8-172Ramberg-Osgood Method, 9-8, 9-188, 9-191Ratioed Values, 1-7Rank Values for A- and B-Basis, 9-267Ratioing of Mechanical Properties, 9-106Reduced Ratios

By Regression, 9-109Direct Computation, 9-106

Reduction in Area, 1-8, 1-11, 9-204Reduction of Column Test Results, 1-31Regression, 9-63, 9-64

Direct Computation, 9-104Determining Design Allowables, 9-65Determining Reduced Ratios, 9-106Example Computations, 9-175Least Squares, 9-67Linear, 9-67Tests for Adequacy of, 9-71Tests for Equality, 9-74Quadratic, 9-68

Rounding, 9-10Runouts, Treatment of, 9-128S-Basis, 1-7, 9-24, 9-59Separately Cast Test Bars, 9-11Shear Failure, 1-28Shear Properties, 1-11, 9-7Shear Test Procedures, 9-106, 9-109Shear Yield Stress, 9-202Significance, A-14Skewness, 9-101

Specific Heat, 9-16Specifying the Population, 9-60Statistics

Symbols, A-5Terms/Definitions, A-6

Strain, 1-8Rate, 1-8Shear, 1-8

Strain Departure Method, 9-194Stress, 1-8, 1-28Stress-Strain Curves, 9-184

Biaxial, 9-198Compression Tangent Modulus, 9-202Data Requirements, 9-31, 9-55Example Computation, 9-198Full-Range, 9-194Presentation, 9-184Typical, 9-184

Stress Rupture, 1-13Symbols and Definitions, 1-3

Creep/Stress Rupture, 9-136, A-7Fatigue, 9-110, A-8Fracture Toughness, 9-133General, 1-3, A-5, A-6Mechanically Fastened Joints, 9-143Mechanical Properties, 9-14Physical Properties, 9-16, 9-183, 9-184Statistics, A-5, A-6

t-Distribution Fractiles, 9-255t-Test, 9-80Tangent Modulus Curves, 9-202Temperature Effects, 1-13, 9-202Tensile Properties, 1-9

Tensile Proportional Limit, 1-9Tensile Ultimate Stress, 1-11Tensile Yield Stress, 1-9

TerminologyCreep Rupture, 9-135Fatigue, 1-15, 9-110Mechanical Property, 9-14

Test Specimens, 9-14Duplication, 9-29Location, 9-14, 9-107Orientation, 9-14Primary Test Direction, 9-15

Testing Procedures, 9-11Bearing, 9-12Creep/Stress Rupture, 9-12, 9-22Elastic Properties, 9-12Fatigue, 9-12, 9-17Fatigue Crack Growth, 9-12, 9-17Fusion-Welded Joints, 9-23Fracture Toughness, 9-18

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MMPDS-0131 January 2003

D-5

Mechanically Fastened Joints, 9-22Mechanical Properties, 9-15Modulus, 9-16Physical Properties, 9-16Shear, 9-13Stress-Strain, 9-28, 9-184Testing Standards, 9-12, 9-15

Tests of Significance, 9-77Definitions, A-6F-Test, 9-79t-Test, 9-80

Thermal Conductivity, 9-16Thermal Exposure, 9-8, 9-208

Complex, 9-210Simple, 9-209

Thin Walled Sections, 1-40Tolerance Bounds, A-15

T90, 9-10T99, 9-10

Tolerance Interval, A-15Tolerance Level, A-15Tolerance Limit Factors

Normal, One-Sided, 9-248Weibull, One-Sided, 9-257, 9-258

Torsion, PropertiesAluminum, 3-521Magnesium, 4-56Steel, 2-240

Typical Basis, 9-8Ultimate Bearing Stress, 1-12Ultimate Compression Stress, 1-1Ultimate Shear Stress, 1-12Ultimate Tensile Stress, 1-11Units, 9-16Weibull Procedure, 9-102Weibull Acceptability Test, 9-83, 9-89Weibull Back-Off, 9-91Weibull Distribution Estimating, 9-89Weibullness, Assessment of, 9-215Weibull Probability Plot, 9-92Wire Rope, 8-172Working Curves, Determination of, 9-202

Yield StressBearing, 1-12Compression, 1-11Shear, 1-12Tensile, 1-9 Tensile Proportional Limit, 1-7

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E-1

APPENDIX E

E.0 Figure IndexFigure No. Current Form Figure No. Current Form

1.4.4.1 Scanned1.4.8.2.1(a) Scanned1.4.8.2.1(b) Scanned1.4.9.3(a) Scanned1.4.11.1 Scanned1.4.11.3 Scanned1.4.12.2 Scanned1.4.12.3 Scanned1.4.12.4 Scanned1.4.12.4.1 Scanned1.4.13.2(a) Scanned1.4.13.2(b) Scanned1.4.13.4 Scanned1.6.2.2 Scanned1.6.4.4(a) Vector Graphic1.6.4.4(b) Vector Graphic1.6.4.4(c) Vector Graphic1.6.4.4(d) Vector Graphic1.6.4.4(e) Vector Graphic1.6.4.4(f) Vector Graphic1.6.4.4(g) Vector Graphic1.6.4.4(h) Vector Graphic1.6.4.4(i) Vector Graphic2.2.1.0 Vector Graphic2.3.0.2 Scanned2.3.1.0 Vector Graphic2.3.1.1.1 Vector Graphic2.3.1.1.2 Vector Graphic2.3.1.1.3 Vector Graphic2.3.1.1.4 Vector Graphic2.3.1.2.6(a) Vector Graphic2.3.1.2.6(b) Vector Graphic2.3.1.2.6(c) Vector Graphic2.3.1.2.8(a) Vector Graphic2.3.1.2.8(b) Vector Graphic2.3.1.2.8(c) Vector Graphic2.3.1.2.8(d) Vector Graphic2.3.1.2.8(e) Vector Graphic2.3.1.2.8(f) Vector Graphic2.3.1.2.8(g) Vector Graphic2.3.1.2.8(h) Vector Graphic2.3.1.3.6(a) Vector Graphic2.3.1.3.6(b) Vector Graphic2.3.1.3.6(c) Vector Graphic

2.3.1.3.6(d) Scanned2.3.1.3.6(e) Vector Graphic2.3.1.3.6(f) Vector Graphic2.3.1.3.6(g) Vector Graphic2.3.1.3.8(a) Vector Graphic2.3.1.3.8(b) Vector Graphic2.3.1.3.8(c) Vector Graphic2.3.1.3.8(d) Vector Graphic2.3.1.3.8(e) Vector Graphic2.3.1.3.8(f) Vector Graphic2.3.1.3.8(g) Vector Graphic2.3.1.3.8(h) Vector Graphic2.3.1.3.8(i) Vector Graphic2.3.1.3.8(j) Vector Graphic2.3.1.3.8(k) Vector Graphic2.3.1.3.8(l) Vector Graphic2.3.1.3.8(m) Vector Graphic2.3.1.3.8(n) Vector Graphic2.3.1.3.8(o) Vector Graphic2.3.1.4.8(a) Scanned2.3.1.4.8(b) Scanned2.3.1.4.8(c) Scanned2.3.1.4.8(d) Scanned2.3.1.4.9 Scanned2.3.1.5.9 Scanned2.4.1.0 Vector Graphic2.4.1.1.1(a) Vector Graphic2.4.1.1.1(b) Vector Graphic2.4.1.1.2(a) Vector Graphic2.4.1.1.2(b) Vector Graphic2.4.1.1.3(a) Vector Graphic2.4.1.1.3(b) Vector Graphic2.4.1.1.4 Vector Graphic2.4.2.0 Vector Graphic2.4.2.1.1 Vector Graphic2.4.2.1.2 Vector Graphic2.4.2.1.4 Vector Graphic2.4.2.1.6(a) Vector Graphic2.4.2.1.6(b) Vector Graphic2.4.3.0 Vector Graphic2.4.3.1.1 Vector Graphic2.4.3.1.2 Vector Graphic

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Figure No. Current Form Figure No. Current Form

E-2

2.4.3.1.3 Vector Graphic2.4.3.1.4 Vector Graphic2.4.3.1.6(a) Vector Graphic2.4.3.1.6(b) Vector Graphic2.4.3.1.6(c) Vector Graphic2.4.3.1.6(d) Vector Graphic2.4.3.1.8 Scanned2.5.0.2(a) Vector Graphic2.5.1.0 Vector Graphic2.5.1.1.1 Vector Graphic2.5.1.1.2 Vector Graphic2.5.1.1.3 Vector Graphic2.5.1.1.4 Vector Graphic2.5.1.1.6(a) Vector Graphic2.5.1.1.6(b) Vector Graphic2.5.1.1.6(c) Vector Graphic2.5.1.1.6(d) Vector Graphic2.5.1.1.6(e) Scanned2.5.2.1.6(a) Vector Graphic2.5.2.1.6(b) Vector Graphic2.5.3.1.6(a) Vector Graphic2.5.3.1.6(b) Vector Graphic2.5.3.1.6(c) Vector Graphic2.5.3.2.6(a) Vector Graphic2.5.3.2.6(b) Vector Graphic2.5.3.2.6(c) Vector Graphic2.6.1.0 Vector Graphic2.6.1.1.1 Vector Graphic2.6.1.1.2 Vector Graphic2.6.1.1.3 Vector Graphic2.6.1.1.4 Vector Graphic2.6.1.1.6(a) Vector Graphic2.6.1.1.6(b) Vector Graphic2.6.2.0 Vector Graphic2.6.2.1.1 Scanned2.6.2.1.2 Vector Graphic2.6.2.1.3 Scanned2.6.2.1.4 Vector Graphic2.6.3.0 Vector Graphic2.6.3.1.1 Vector Graphic2.6.3.1.2 Vector Graphic2.6.3.1.5 Vector Graphic2.6.3.1.6 Vector Graphic2.6.3.1.8 Scanned2.6.3.2.1 Vector Graphic2.6.3.2.2 Vector Graphic2.6.3.2.5 Vector Graphic2.6.3.2.6 Vector Graphic2.6.3.2.8 Scanned

2.6.4.0 Vector Graphic2.6.4.1.1 Vector Graphic2.6.4.1.2 Vector Graphic2.6.4.1.5 Vector Graphic2.6.4.1.6 Vector Graphic2.6.4.1.8(a) Scanned2.6.4.1.8(b) Scanned2.6.4.2.1 Vector Graphic2.6.4.2.2 Vector Graphic2.6.4.2.5 Scanned2.6.4.2.6 Vector Graphic2.6.4.2.8 Scanned2.6.5.0(a) Vector Graphic2.6.5.1(a) Vector Graphic2.6.5.1(b) Vector Graphic2.6.5.1(c) Vector Graphic2.6.6.0 Vector Graphic2.6.6.1.1 Vector Graphic2.6.6.1.6(a) Vector Graphic2.6.6.1.6(b) Vector Graphic2.6.6.1.6(c) Vector Graphic2.6.6.1.8(a) Vector Graphic2.6.6.1.8(b) Vector Graphic2.6.6.1.8(c) Vector Graphic2.6.7.0 Vector Graphic2.6.7.1.1 Vector Graphic2.6.7.1.4 Vector Graphic2.6.7.1.6(a) Vector Graphic2.6.7.1.6(b) Scanned2.6.7.1.6(c) Vector Graphic2.6.7.2.2 Vector Graphic2.6.7.2.6(a) Scanned2.6.7.2.6(b) Vector Graphic2.6.7.2.8(a) Vector Graphic2.6.7.2.8(b) Vector Graphic2.6.7.2.8(c) Vector Graphic2.6.7.3.2 Scanned2.6.7.3.6 Scanned2.6.8.0 Vector Graphic2.6.8.1.1 Scanned2.6.8.1.4 Scanned2.6.8.1.6(a) Scanned2.6.8.1.6(b) Scanned2.6.8.1.6(c) Scanned2.6.8.1.8(a) Scanned2.6.8.1.8(b) Scanned2.6.8.1.8(c) Scanned2.6.8.1.8(d) Scanned2.6.8.1.8(e) Vector Graphic

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Figure No. Current Form Figure No. Current Form

E-3

2.6.8.1.8(f) Scanned2.6.9.0 Vector Graphic2.6.9.1.2 Vector Graphic2.6.9.1.3 Vector Graphic2.6.9.1.4 Vector Graphic2.6.9.1.8(a) Scanned2.6.9.1.8(b) Scanned2.6.9.1.8(c) Scanned2.6.9.2.1 Vector Graphic2.6.9.2.6(a) Vector Graphic2.6.9.2.6(b) Vector Graphic2.6.9.3.6(a) Vector Graphic2.6.9.3.6(b) Vector Graphic2.6.9.4.8 Scanned2.6.9.5.8 Scanned2.6.9.6.1 Vector Graphic2.6.10.0 Vector Graphic2.6.10.1.1 Vector Graphic2.6.10.1.2 Vector Graphic2.6.10.1.4(a) Vector Graphic2.6.10.1.4(b) Vector Graphic2.6.10.1.6(a) Vector Graphic2.6.10.1.6(b) Vector Graphic2.6.10.1.6(c) Vector Graphic2.7.1.0 Vector Graphic2.7.1.1.1(a) Vector Graphic2.7.1.1.1(b) Vector Graphic2.7.1.2.6(a) Vector Graphic2.7.1.2.6(b) Vector Graphic2.7.1.3.1 Vector Graphic2.7.1.3.2 Vector Graphic2.7.1.3.3 Vector Graphic2.7.1.3.4 Vector Graphic2.7.1.3.6(a) Vector Graphic2.7.1.3.6(b) Vector Graphic2.7.1.4.6(a) Vector Graphic2.7.1.4.6(b) Vector Graphic2.7.1.5.1 Vector Graphic2.7.1.5.2(a) Vector Graphic2.7.1.5.2(b) Vector Graphic2.7.1.5.3 Vector Graphic2.7.1.5.4 Vector Graphic2.7.1.5.6(a) Vector Graphic2.7.1.5.6(b) Vector Graphic2.7.1.5.6(c) Vector Graphic2.7.1.5.6(d) Vector Graphic2.8.1.1(a) Vector Graphic2.8.1.1(b) Vector Graphic2.8.3.2(a) Vector Graphic

2.8.3.2(b) Vector Graphic2.8.3.2(c) Vector Graphic2.8.3.2(d) Scanned2.8.3.2(e) Scanned2.8.3.2(f) Vector Graphic2.8.3.2(g) Scanned2.8.3.2(h) Scanned2.8.3.2(i) Vector Graphic2.8.3.2(j) Scanned3.1.2.1.1(a) Scanned3.1.2.1.1(b) Scanned3.1.2.1.1(c) Scanned3.2.1.0 Vector Graphic3.2.1.1.1(a) Scanned3.2.1.1.1(b) Vector Graphic3.2.1.1.1(c) Vector Graphic3.2.1.1.1(d) Vector Graphic3.2.1.1.1(e) Vector Graphic3.2.1.1.1(f) Vector Graphic3.2.1.1.2(a) Vector Graphic3.2.1.1.2(b) Vector Graphic3.2.1.1.3(a) Vector Graphic3.2.1.1.3(b) Vector Graphic3.2.1.1.4 Scanned3.2.1.1.5(a) Vector Graphic3.2.1.1.5(b) Vector Graphic3.2.1.1.6(a) Vector Graphic3.2.1.1.6(b) Vector Graphic3.2.1.1.6(c) Vector Graphic3.2.1.1.6(d) Vector Graphic3.2.1.1.6(e) Vector Graphic3.2.1.1.6(f) Vector Graphic3.2.1.1.6(g) Vector Graphic3.2.1.1.6(h) Vector Graphic3.2.1.1.6(i) Vector Graphic3.2.1.1.6(j) Vector Graphic3.2.1.1.6(k) Vector Graphic3.2.1.1.6(l) Vector Graphic3.2.1.1.6(m) Vector Graphic3.2.1.1.6(n) Vector Graphic3.2.1.1.6(o) Vector Graphic3.2.1.1.6(p) Vector Graphic3.2.1.1.6(q) Vector Graphic3.2.1.1.6(r) Vector Graphic3.2.1.1.6(s) Vector Graphic3.2.1.1.6(t) Vector Graphic3.2.1.1.6(u) Vector Graphic3.2.1.1.6(v) Vector Graphic3.2.1.1.8(a) Scanned

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Figure No. Current Form Figure No. Current Form

E-4

3.2.1.1.8(b) Vector Graphic3.2.1.1.8(c) Vector Graphic3.2.1.1.8(d) Vector Graphic3.2.1.1.8(e) Vector Graphic3.2.2.0 Vector Graphic3.2.2.1.4 Vector Graphic3.2.3.0 Vector Graphic3.2.3.1.1(a) Vector Graphic3.2.3.1.1(b) Vector Graphic3.2.3.1.1(c) Vector Graphic3.2.3.1.1(d) Vector Graphic3.2.3.1.1(e) Vector Graphic3.2.3.1.1(f) Vector Graphic3.2.3.1.2(a) Vector Graphic3.2.3.1.2(b) Vector Graphic3.2.3.1.3(a) Vector Graphic3.2.3.1.3(b) Vector Graphic3.2.3.1.4 Scanned3.2.3.1.5(a) Vector Graphic3.2.3.1.5(b) Vector Graphic3.2.3.1.6(a) Vector Graphic3.2.3.1.6(b) Vector Graphic3.2.3.1.6(c) Vector Graphic3.2.3.1.6(d) Vector Graphic3.2.3.1.6(e) Vector Graphic3.2.3.1.6(f) Vector Graphic3.2.3.1.6(g) Vector Graphic3.2.3.1.6(h) Vector Graphic3.2.3.1.6(i) Vector Graphic3.2.3.1.6(j) Vector Graphic3.2.3.1.6(k) Vector Graphic3.2.3.1.6(l) Vector Graphic3.2.3.1.6(m) Vector Graphic3.2.3.1.6(n) Vector Graphic3.2.3.1.6(o) Vector Graphic3.2.3.1.6(p) Vector Graphic3.2.3.1.6(q) Vector Graphic3.2.3.1.6(r) Vector Graphic3.2.3.1.6(s) Vector Graphic3.2.3.1.6(t) Vector Graphic3.2.3.1.6(u) Vector Graphic3.2.3.1.6(v) Vector Graphic3.2.3.1.6(w) Vector Graphic3.2.3.1.6(x) Vector Graphic3.2.3.1.6(y) Vector Graphic3.2.3.1.6(z) Vector Graphic3.2.3.1.6(aa) Vector Graphic3.2.3.1.8(a) Scanned3.2.3.1.8(b) Vector Graphic

3.2.3.1.8(c) Vector Graphic3.2.3.1.8(d) Vector Graphic3.2.3.1.8(e) Scanned3.2.3.1.8(f) Vector Graphic3.2.3.1.8(g) Vector Graphic3.2.3.1.8(h) Vector Graphic3.2.3.1.8(i) Vector Graphic3.2.3.3.1(a) Vector Graphic3.2.3.3.1(b) Vector Graphic3.2.3.3.1(c) Vector Graphic3.2.3.3.1(d) Vector Graphic3.2.3.3.5(a) Vector Graphic3.2.3.3.5(b) Vector Graphic3.2.3.3.6(a) Vector Graphic3.2.3.3.6(b) Vector Graphic3.2.3.3.6(c) Vector Graphic3.2.3.3.6(d) Vector Graphic3.2.3.3.6(e) Vector Graphic3.2.3.4.1(a) Vector Graphic3.2.3.4.1(b) Vector Graphic3.2.3.4.1(c) Vector Graphic3.2.3.4.1(d) Vector Graphic3.2.3.4.1(e) Scanned3.2.3.4.1(f) Scanned3.2.3.4.2(a) Vector Graphic3.2.3.4.2(b) Vector Graphic3.2.3.4.3(a) Vector Graphic3.2.3.4.3(b) Vector Graphic3.2.3.4.5(a) Vector Graphic3.2.3.4.5(b) Vector Graphic3.2.3.4.6(a) Vector Graphic3.2.3.4.6(b) Vector Graphic3.2.3.4.6(c) Vector Graphic3.2.3.4.6(d) Vector Graphic3.2.3.4.6(e) Vector Graphic3.2.3.4.6(f) Vector Graphic3.2.3.4.6(g) Vector Graphic3.2.3.4.6(h) Vector Graphic3.2.3.4.6(i) Vector Graphic3.2.3.4.6(j) Vector Graphic3.2.3.5.1(a) Vector Graphic3.2.3.5.1(b) Vector Graphic3.2.3.5.1(c) Vector Graphic3.2.3.5.1(d) Vector Graphic3.2.3.5.2(a) Vector Graphic3.2.3.5.2(b) Vector Graphic3.2.3.5.3(a) Vector Graphic3.2.3.5.3(b) Vector Graphic3.2.3.5.3(c) Vector Graphic

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Figure No. Current Form Figure No. Current Form

E-5

3.2.3.5.5(a) Scanned3.2.3.5.5(b) Scanned3.2.3.5.6(a) Vector Graphic3.2.3.5.6(b) Vector Graphic3.2.3.5.6(c) Vector Graphic3.2.3.5.6(d) Vector Graphic3.2.3.5.10(a) Scanned3.2.3.5.10(b) Scanned3.2.4.0 Vector Graphic3.2.6.1.6(a) Vector Graphic3.2.6.1.6(b) Vector Graphic3.2.7.1.1(a) Vector Graphic3.2.7.1.1(b) Vector Graphic3.2.7.1.6(a) Scanned3.2.7.1.6(b) Scanned3.2.7.1.9(a) Scanned3.2.7.1.9(b) Scanned3.2.7.1.9(c) Scanned3.2.7.1.9(d) Scanned3.2.7.1.9(e) Scanned3.2.8.0 Vector Graphic3.2.8.1.1(a) Vector Graphic3.2.8.1.1(b) Vector Graphic3.2.8.1.6(a) Vector Graphic3.2.8.1.6(b) Vector Graphic3.2.8.2.1(a) Vector Graphic3.2.8.2.1(b) Vector Graphic3.2.8.2.6(a) Vector Graphic3.2.8.2.6(b) Vector Graphic3.2.8.2.8(a) Scanned3.2.8.2.8(b) Scanned3.2.8.2.8(c) Scanned3.2.8.2.8(d) Scanned3.2.8.3.6(a) Vector Graphic3.2.8.3.6(b) Vector Graphic3.2.8.3.6(c) Vector Graphic3.2.8.3.6(d) Vector Graphic3.2.8.3.6(e) Vector Graphic3.2.8.4.1(a) Vector Graphic3.2.8.4.1(b) Vector Graphic3.2.8.4.6(a) Vector Graphic3.2.8.4.6(b) Vector Graphic3.2.8.4.6(c) Vector Graphic3.2.8.4.6(d) Vector Graphic3.2.8.4.6(e) Vector Graphic3.2.10.1.6(a) Vector Graphic3.2.10.1.6(b) Vector Graphic3.2.11.1.6(a) Vector Graphic3.2.11.1.6(b) Vector Graphic

3.2.11.1.6(c) Vector Graphic3.2.12.0 Vector Graphic3.2.12.1.1(a) Vector Graphic3.2.12.1.1(b) Vector Graphic3.2.12.1.1(c) Vector Graphic3.2.12.1.1(d) Vector Graphic3.2.12.1.2 Vector Graphic3.2.12.1.3 Vector Graphic3.2.12.1.4 Vector Graphic3.2.12.1.5 Vector Graphic3.2.12.1.6(a) Vector Graphic3.2.12.1.6(b) Vector Graphic3.5.1.0 Vector Graphic3.5.1.1.1 Vector Graphic3.5.1.1.4 Vector Graphic3.5.1.1.5 Vector Graphic3.5.1.3.1(a) Vector Graphic3.5.1.3.1(b) Vector Graphic3.5.1.3.1(c) Vector Graphic3.5.1.3.1(d) Vector Graphic3.5.1.3.5(a) Vector Graphic3.5.1.3.5(b) Vector Graphic3.5.1.5.1(a) Vector Graphic3.5.1.5.1(b) Vector Graphic3.5.1.5.1(c) Vector Graphic3.5.1.5.1(d) Vector Graphic3.5.1.5.5(a) Vector Graphic3.5.1.5.5(b) Vector Graphic3.5.2.0 Vector Graphic3.5.2.1.6(a) Vector Graphic3.5.2.1.6(b) Vector Graphic3.5.2.1.6(c) Vector Graphic3.5.3.1.6(a) Vector Graphic3.5.3.1.6(b) Vector Graphic3.5.3.1.6(c) Vector Graphic3.5.3.2.6(a) Vector Graphic3.5.3.2.6(b) Vector Graphic3.5.3.2.6(c) Vector Graphic3.5.3.3.6(a) Vector Graphic3.5.3.3.6(b) Vector Graphic3.5.3.3.6(c) Vector Graphic3.5.3.4.6 Vector Graphic3.5.3.7.6 Vector Graphic3.5.4.1.6 Vector Graphic3.5.4.2.6 Vector Graphic3.5.4.3.6(a) Vector Graphic3.5.4.3.6(b) Vector Graphic3.5.5.0 Vector Graphic3.5.5.1.6(a) Vector Graphic

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Figure No. Current Form Figure No. Current Form

E-6

3.5.5.1.6(b) Vector Graphic3.5.5.2.6 Vector Graphic3.5.5.4.6 Vector Graphic3.6.1.1.6(a) Vector Graphic3.6.1.1.6(b) Vector Graphic3.6.2.0 Vector Graphic3.6.2.2.1(a) Vector Graphic3.6.2.2.1(b) Vector Graphic3.6.2.2.1(c) Vector Graphic3.6.2.2.1(d) Vector Graphic3.6.2.2.4 Vector Graphic3.6.2.2.5(a) Vector Graphic3.6.2.2.5(b) Vector Graphic3.6.2.2.6(a) Vector Graphic3.6.2.2.6(b) Vector Graphic3.6.2.2.6(c) Vector Graphic3.6.2.2.6(d) Vector Graphic3.6.2.2.6(e) Vector Graphic3.6.2.2.6(f) Vector Graphic3.6.2.2.6(g) Vector Graphic3.6.2.2.6(h) Vector Graphic3.6.2.2.6(i) Vector Graphic3.6.2.2.6(j) Vector Graphic3.6.2.2.6(k) Vector Graphic3.6.2.2.6(l) Vector Graphic3.6.2.2.6(m) Vector Graphic3.6.2.2.6(n) Vector Graphic3.6.2.2.6(o) Vector Graphic3.6.2.2.8 Vector Graphic3.6.3.0 Vector Graphic3.7.1.1.1 Vector Graphic3.7.1.1.6(a) Vector Graphic3.7.1.1.6(b) Vector Graphic3.7.1.1.6(c) Vector Graphic3.7.1.1.6(d) Vector Graphic3.7.1.2.6(a) Vector Graphic3.7.1.2.6(b) Vector Graphic3.7.1.2.6(c) Vector Graphic3.7.1.2.6(d) Vector Graphic3.7.2.0 Vector Graphic3.7.3.1.1 Vector Graphic3.7.3.1.6(a) Vector Graphic3.7.3.1.6(b) Vector Graphic3.7.3.1.6(c) Vector Graphic3.7.3.1.6(d) Vector Graphic3.7.3.1.6(e) Vector Graphic3.7.3.1.6(f) Vector Graphic3.7.3.1.6(g) Vector Graphic3.7.3.1.8(a) Scanned

3.7.3.1.8(b) Scanned3.7.3.1.8(c) Scanned3.7.3.1.8(d) Scanned3.7.3.1.8(e) Scanned3.7.3.1.8(f) Scanned3.7.3.1.8(g) Scanned3.7.4.1.6(a) Vector Graphic3.7.4.1.6(b) Vector Graphic3.7.4.1.6(c) Vector Graphic3.7.4.1.6(d) Vector Graphic3.7.4.1.8(a) Scanned3.7.4.1.8(b) Scanned3.7.4.2.1 Vector Graphic3.7.4.2.6(a) Vector Graphic3.7.4.2.6(b) Vector Graphic3.7.4.2.6(c) Vector Graphic3.7.4.2.6(d) Vector Graphic3.7.4.2.6(e) Vector Graphic3.7.4.2.6(f) Vector Graphic3.7.4.2.6(g) Vector Graphic3.7.4.2.6(h) Vector Graphic3.7.4.2.6(i) Vector Graphic3.7.4.2.6(j) Vector Graphic3.7.4.2.8(a) Scanned3.7.4.2.8(b) Vector Graphic3.7.4.2.8(c) Vector Graphic3.7.4.2.8(d) Vector Graphic3.7.4.2.8(e) Scanned3.7.4.2.8(f) Scanned3.7.4.2.8(g) Scanned3.7.4.2.8(h) Scanned3.7.4.2.8(i) Scanned3.7.4.2.8(j) Scanned3.7.4.2.8(k) Scanned3.7.4.2.8(l) Scanned3.7.4.2.9(a) Scanned3.7.4.2.9(b) Scanned3.7.4.2.9(c) Scanned3.7.4.3.6(a) Vector Graphic3.7.4.3.6(b) Vector Graphic3.7.4.3.6(c) Vector Graphic3.7.4.3.6(d) Vector Graphic3.7.4.3.6(e) Vector Graphic3.7.4.3.6(f) Vector Graphic3.7.4.3.8(a) Scanned3.7.4.3.8(b) Scanned3.7.6.0 Vector Graphic3.7.6.1.1(a) Scanned3.7.6.1.1(b) Scanned

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Figure No. Current Form Figure No. Current Form

E-7

3.7.6.1.1(c) Vector Graphic3.7.6.1.1(d) Vector Graphic3.7.6.1.2(a) Vector Graphic3.7.6.1.2(b) Vector Graphic3.7.6.1.3(a) Vector Graphic3.7.6.1.3(b) Vector Graphic3.7.6.1.4 Vector Graphic3.7.6.1.5(a) Vector Graphic3.7.6.1.5(b) Vector Graphic3.7.6.1.6(a) Vector Graphic3.7.6.1.6(b) Vector Graphic3.7.6.1.6(c) Vector Graphic3.7.6.1.6(d) Vector Graphic3.7.6.1.6(e) Vector Graphic3.7.6.1.6(f) Vector Graphic3.7.6.1.6(g) Vector Graphic3.7.6.1.6(h) Vector Graphic3.7.6.1.6(i) Vector Graphic3.7.6.1.6(j) Vector Graphic3.7.6.1.6(k) Vector Graphic3.7.6.1.6(l) Vector Graphic3.7.6.1.6(m) Vector Graphic3.7.6.1.6(n) Vector Graphic3.7.6.1.6(o) Vector Graphic3.7.6.1.6(p) Vector Graphic3.7.6.1.6(q) Vector Graphic3.7.6.1.8(a) Scanned3.7.6.1.8(b) Scanned3.7.6.1.8(c) Scanned3.7.6.1.8(d) Vector Graphic3.7.6.1.8(e) Scanned3.7.6.1.8(f) Vector Graphic3.7.6.1.8(g) Scanned3.7.6.1.8(h) Vector Graphic3.7.6.1.9 Scanned3.7.6.1.10(a) Scanned3.7.6.1.10(b) Scanned3.7.6.1.10(c) Scanned3.7.6.1.10(d) Scanned3.7.6.1.10(e) Scanned3.7.6.1.10(f) Scanned3.7.6.1.10(g) Scanned3.7.6.1.10(h) Scanned3.7.6.2.6(a) Vector Graphic3.7.6.2.6(b) Vector Graphic3.7.6.2.6(c) Vector Graphic3.7.6.2.6(d) Vector Graphic3.7.6.2.6(e) Vector Graphic3.7.6.2.6(f) Vector Graphic

3.7.6.2.9(a) Scanned3.7.6.2.9(b) Scanned3.7.6.2.9(c) Scanned3.7.6.2.10(a) Scanned3.7.6.2.10(b) Scanned3.7.7.1.6(a) Vector Graphic3.7.7.1.6(b) Vector Graphic3.7.7.1.6(c) Vector Graphic3.7.7.1.6(d) Vector Graphic3.7.7.2.6(a) Vector Graphic3.7.7.2.6(b) Vector Graphic3.7.7.2.6(c) Vector Graphic3.7.7.2.6(d) Vector Graphic3.7.7.2.8(a) Vector Graphic3.7.7.2.8(b) Vector Graphic3.7.7.2.8(c) Vector Graphic3.7.8.1.6(a) Vector Graphic3.7.8.1.6(b) Vector Graphic3.7.8.1.8(a) Vector Graphic 3.7.8.1.8(b) Vector Graphic3.7.8.1.8(c) Vector Graphic3.7.8.1.8(d) Vector Graphic3.7.8.2.6(a) Vector Graphic3.7.8.2.6(b) Vector Graphic3.7.8.2.6(c) Vector Graphic3.7.8.2.6(d) Vector Graphic3.7.8.2.6(e) Vector Graphic3.7.8.2.6(f) Vector Graphic3.7.8.2.8(a) Scanned3.7.8.2.8(b) Scanned3.7.9.1.6(a) Vector Graphic3.7.9.1.6(b) Vector Graphic3.7.9.1.6(c) Vector Graphic3.7.10.1.6(a) Vector Graphic3.7.10.1.6(b) Vector Graphic3.7.10.1.6(c) Vector Graphic3.7.10.1.6(d) Vector Graphic3.7.10.1.6(e) Vector Graphic3.7.10.1.6(f) Vector Graphic3.7.10.1.6(g) Vector Graphic3.7.10.1.8(a) Scanned3.7.10.1.8(b) Vector Graphic3.7.10.1.8(c) Scanned3.7.10.1.10(a) Scanned3.7.10.1.10(b) Scanned3.7.10.1.10(c) Scanned3.7.10.1.10(d) Scanned3.7.10.2.6(a) Vector Graphic3.7.10.2.6(b) Vector Graphic

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Figure No. Current Form Figure No. Current Form

E-8

3.7.10.2.8(a) Scanned3.7.10.2.8(b) Scanned3.7.10.2.9(a) Scanned3.7.10.2.9(b) Scanned3.7.10.3.6(a) Vector Graphic3.7.10.3.6(b) Vector Graphic3.7.10.3.6(c) Vector Graphic3.7.10.3.6(d) Vector Graphic3.7.10.3.6(e) Vector Graphic3.7.10.3.6(f) Vector Graphic3.7.10.3.6(g) Vector Graphic3.7.10.3.6(h) Vector Graphic3.7.10.3.6(i) Vector Graphic3.7.10.3.6(j) Vector Graphic3.7.10.3.6(k) Vector Graphic3.7.10.3.6(l) Vector Graphic3.7.10.3.10(a) Scanned3.7.10.3.10(b) Scanned3.8.1.0 Vector Graphic3.8.1.1.6 Vector Graphic3.8.1.1.8(a) Scanned3.8.1.1.8(b) Scanned3.8.1.1.8(c) Scanned3.9.2.0 Vector Graphic3.9.4.0 Vector Graphic3.9.5.1.6(a) Vector Graphic3.9.5.1.6(b) Vector Graphic3.9.6.1.6 Vector Graphic3.9.7.1.6 Vector Graphic3.10.1.1.1 Vector Graphic3.10.2.3(a) Scanned3.10.2.3(b) Scanned3.10.3.2(a) Scanned3.10.3.2(b) Vector Graphic3.10.3.2(c) Scanned3.10.3.2(d) Scanned3.10.3.2(e) Vector Graphic3.10.3.2(f) Vector Graphic3.10.3.2(g) Vector Graphic4.2.1.0 Vector Graphic4.2.1.1.4 Scanned4.2.1.1.6 Vector Graphic4.2.1.2.1 Scanned4.2.1.2.2 Scanned4.2.1.2.3 Scanned4.2.1.2.4 Scanned4.2.1.2.6 Vector Graphic4.2.1.4.8(a) Vector Graphic4.2.1.4.8(b) Scanned

4.2.3.0 Vector Graphic4.2.3.2.6(a) Vector Graphic4.2.3.2.6(b) Scanned4.2.3.2.8(a) Scanned4.2.3.2.8(b) Scanned4.2.3.2.8(c) Scanned4.3.2.1.4 Vector Graphic4.3.2.1.6 Vector Graphic4.3.3.0 Vector Graphic4.3.3.1.1(a) Vector Graphic4.3.3.1.1(b) Vector Graphic4.3.3.1.1(c) Vector Graphic4.3.3.1.4 Vector Graphic4.3.3.1.6(a) Vector Graphic4.3.3.1.6(b) Vector Graphic4.3.4.0 Vector Graphic4.3.4.1.1(a) Scanned4.3.4.1.1(b) Scanned4.3.4.1.1(C) Scanned4.3.4.1.6 Vector Graphic4.3.5.1.1 Scanned4.3.5.1.4 Scanned4.3.5.1.6 Vector Graphic4.3.6.0 Scanned4.3.6.1.1 Scanned4.3.6.1.4 Scanned4.3.6.1.6(a) Scanned4.3.6.1.6(b) Vector Graphic4.4.2.3(a) Scanned4.4.2.3(b) Scanned4.4.3.2 Scanned5.2.1.0 Scanned5.2.1.1.1(a) Scanned5.2.1.1.1(b) Scanned5.2.1.1.2(a) Scanned5.2.1.1.2(b) Scanned5.2.1.1.3(a) Scanned5.2.1.1.3(b) Scanned5.2.1.1.6(a) Scanned5.2.1.1.6(b) Scanned5.3.1.0 Vector Graphic5.3.1.1.1 Scanned5.3.1.1.2 Scanned5.3.1.1.3 Scanned5.3.1.1.4 Scanned5.3.1.1.5 Scanned5.3.1.1.9(a) Scanned5.3.1.1.9(b) Scanned5.3.1.1.9(c) Scanned

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Figure No. Current Form Figure No. Current Form

E-9

5.3.2.0 Scanned5.3.2.1.1 Scanned5.3.2.1.4 Scanned5.3.2.1.6(a) Vector Graphic5.3.2.1.6(b) Vector Graphic5.3.2.2.1 Scanned5.3.2.2.6(a) Vector Graphic5.3.2.2.6(b) Vector Graphic5.3.2.2.8(a) Scanned5.3.2.2.8(b) Scanned5.3.2.2.8(c) Scanned5.3.2.2.8(d) Scanned5.3.2.2.8(e) Scanned5.3.2.2.8(f) Scanned5.3.3.0 Scanned5.3.3.1.1 Scanned5.3.3.1.2 Scanned5.3.3.1.4 Scanned5.3.3.1.6(a) Vector Graphic5.3.3.1.6(b) Vector Graphic5.3.3.1.6(c) Scanned5.4.1.0 Vector Graphic5.4.1.1.1 Vector Graphic5.4.1.1.2 Scanned5.4.1.1.3 Scanned5.4.1.1.4 Scanned5.4.1.1.5 Scanned5.4.1.1.6(a) Vector Graphic5.4.1.1.6(b) Vector Graphic5.4.1.1.6(c) Vector Graphic5.4.1.1.6(d) Scanned5.4.1.1.8(a) Scanned5.4.1.1.8(b) Scanned5.4.1.1.8(c) Scanned5.4.1.1.8(d) Scanned5.4.1.1.8(e) Scanned5.4.1.1.8(f) Scanned5.4.1.1.8(g) Scanned5.4.1.1.9 Scanned5.4.1.2.1 Scanned5.4.1.2.2 Scanned5.4.1.2.3 Scanned5.4.1.2.4 Scanned5.4.1.2.6(a) Vector Graphic5.4.1.2.6(b) Vector Graphic5.4.1.2.6(c) Vector Graphic5.4.1.2.6(d) Vector Graphic5.4.1.2.6(e) Vector Graphic5.4.1.2.6(f) Vector Graphic

5.4.1.2.6(g) Vector Graphic5.4.1.2.6(h) Scanned5.4.1.2.7 Scanned5.4.1.2.8(a) Scanned5.4.1.2.8(b) Scanned5.4.1.2.8(c) Scanned5.4.1.2.8(d) Scanned5.4.1.2.8(e) Scanned5.4.1.2.8(f) Scanned5.4.1.2.8(g) Scanned5.4.1.2.8(h) Scanned5.4.1.2.8(i) Scanned5.4.2.0 Scanned5.4.2.1.1(a) Scanned5.4.2.1.1(b) Scanned5.4.2.1.2(a) Scanned5.4.2.1.2(b) Scanned5.4.2.1.3(a) Scanned5.4.2.1.3(b) Scanned5.4.2.1.6(a) Vector Graphic5.4.2.1.6(b) Vector Graphic5.4.2.1.6(c) Scanned5.4.2.1.8(a) Scanned5.4.2.1.8(b) Scanned5.4.2.2.1 Scanned5.4.2.2.2 Scanned5.4.3.1(a) Vector Graphic5.4.3.1(b) Vector Graphic5.4.3.1(c) Vector Graphic5.4.3.2(a) Scanned5.4.3.2(b) Scanned5.4.3.3 Scanned5.5.1.0 Scanned5.5.1.1.1 Scanned5.5.1.1.2 Scanned5.5.1.1.3(a) Scanned5.5.1.1.3(b) Scanned5.5.1.1.4 Scanned5.5.1.1.6 Vector Graphic5.5.1.1.8(a) Scanned5.5.1.1.8(b) Scanned5.5.1.1.8(c) Scanned5.5.1.1.8(d) Scanned5.5.1.2.1 Scanned5.5.1.2.2 Scanned5.5.1.2.3 Scanned5.5.1.2.4 Scanned5.5.1.2.6 Vector Graphic5.5.1.2.8(a) Scanned

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Figure No. Current Form Figure No. Current Form

E-10

5.5.1.2.8(b) Scanned5.5.1.2.8(c) Scanned5.5.2.0 Scanned5.5.2.1.6(a) Vector Graphic5.5.2.1.6(b) Vector Graphic5.5.3.1.6 Vector Graphic5.5.3.2.6 Vector Graphic5.6.1.1.1 Scanned6.2.1.0 Scanned6.2.1.1.1 Scanned6.2.1.1.3 Scanned6.2.1.1.4(a) Scanned6.2.1.1.4(b) Scanned6.2.1.1.4(c) Scanned6.2.1.1.8(a) Scanned6.2.1.1.8(b) Scanned6.2.1.1.8(c) Scanned6.2.1.1.8(d) Scanned6.2.1.1.8(e) Scanned6.2.2.0 Scanned6.2.2.1.1(a) Scanned6.2.2.1.1(b) Scanned6.2.2.1.4(a) Scanned6.2.2.1.4(b) Scanned6.3.1.0 Scanned6.3.1.1.1 Scanned6.3.1.1.4 Scanned6.3.1.1.6(a) Vector Graphic6.3.1.1.6(b) Vector Graphic6.3.2.0 Scanned6.3.2.1.1 Scanned6.3.2.1.2 Scanned6.3.2.1.3 Scanned6.3.2.1.4 Scanned6.3.3.0 Scanned6.3.3.1.1(a) Scanned6.3.3.1.1(b) Scanned6.3.3.1.4(a) Scanned6.3.3.1.4(b) Scanned6.3.3.1.6(a) Vector Graphic6.3.3.1.6(b) Vector Graphic6.3.3.1.6(c) Vector Graphic6.3.3.1.6(d) Vector Graphic6.3.3.1.8(a) Scanned6.3.3.1.8(b) Scanned6.3.3.1.8(c) Scanned6.3.3.1.8(d) Scanned6.3.4.0 Vector Graphic6.3.4.1.1 Vector Graphic

6.3.4.1.4 Vector Graphic6.3.4.1.5 Vector Graphic6.3.4.1.6(a) Vector Graphic6.3.4.1.6(b) Vector Graphic6.3.4.1.6(c) Scanned6.3.5.0 Vector Graphic6.3.5.1.1 Scanned6.3.5.1.4(a) Scanned6.3.5.1.4(b) Scanned6.3.5.1.4(c) Scanned6.3.5.1.6(a) Vector Graphic6.3.5.1.6(b) Vector Graphic6.3.5.1.6(c) Vector Graphic6.3.5.1.6(d) Scanned6.3.5.1.7(a) Scanned6.3.5.1.7(b) Scanned6.3.5.1.7(c) Scanned6.3.5.1.7(d) Vector Graphic6.3.5.1.7(e) Vector Graphic6.3.5.1.8(a) Vector Graphic6.3.5.1.8(b) Vector Graphic6.3.5.1.8(c) Vector Graphic6.3.5.1.8(d) Vector Graphic6.3.5.1.8(e) Vector Graphic6.3.5.1.8(f) Vector Graphic6.3.5.1.8(g) Vector Graphic6.3.5.1.9(a) Vector Graphic6.3.5.1.9(b) Scanned6.3.5.1.9(c) Scanned6.3.6.0 Scanned6.3.6.1.1 Scanned6.3.6.1.2 Scanned6.3.6.1.3 Scanned6.3.6.2.1(a) Scanned6.3.6.2.1(b) Scanned6.3.6.2.4(a) Scanned6.3.6.2.4(b) Scanned6.3.7.0 Scanned6.3.7.1.1 Vector Graphic6.3.7.1.2 Vector Graphic6.3.7.1.3(a) Scanned6.3.7.1.3(b) Scanned6.3.7.1.4 Scanned6.3.7.1.5 Scanned6.3.7.1.7 Scanned6.3.8.0 Scanned6.3.8.1.1 Scanned6.3.8.1.4 Scanned6.3.8.1.5(a) Scanned

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Figure No. Current Form Figure No. Current Form

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6.3.8.1.5(b) Scanned6.3.8.1.6(a) Scanned6.3.8.1.6(b) Scanned6.3.9.0(a) Vector Graphic6.3.9.0(b) Vector Graphic6.3.9.0(c) Vector Graphic6.3.9.1.1(a) Vector Graphic6.3.9.1.1(b) Vector Graphic6.3.9.1.4 Vector Graphic6.3.9.1.5 Vector Graphic6.3.9.1.6(a) Vector Graphic6.3.9.1.6(b) Vector Graphic6.3.9.1.6(c ) Vector Graphic6.3.9.1.6(d ) Vector Graphic6.3.9.1.6(e ) Vector Graphic6.3.9.1.6(f ) Vector Graphic6.3.9.1.6(g ) Vector Graphic6.3.9.1.6(h) Vector Graphic6.3.9.1.6(i) Vector Graphic6.3.10.0(a) Vector Graphic6.3.10.0(b) Vector Graphic6.3.10.0(c) Vector Graphic6.3.10.0(d) Vector Graphic6.3.10.1.1(a) Vector Graphic6.3.10.1.7(a) Vector Graphic6.3.10.1.7(b) Vector Graphic6.4.1.0 Scanned6.4.1.1.1 Vector Graphic6.4.1.1.2 Vector Graphic6.4.1.1.3 Vector Graphic6.4.1.1.4(a) Vector Graphic6.4.1.1.4(b) Scanned6.4.1.1.5 Scanned6.4.1.1.7 Scanned6.4.2.0 Scanned6.4.2.1.1(a) Scanned6.4.2.1.1(b) Scanned6.4.2.1.2 Scanned6.4.2.1.4(a) Scanned6.4.2.1.4(b) Scanned6.4.2.1.4(c) Scanned6.4.2.1.5 Scanned6.4.2.1.6(a) Vector Graphic6.4.2.1.6(b) Vector Graphic6.4.2.1.8(a) Scanned6.4.2.1.8(b) Scanned6.4.2.1.8(c) Scanned6.4.2.1.8(d) Scanned7.2.1.0 Vector Graphic

7.2.1.1.1 Vector Graphic7.2.1.1.4 Vector Graphic7.3.2.0 Vector Graphic7.3.2.1.6(a) Vector Graphic7.3.2.1.6(b) Vector Graphic7.3.2.2.6 Vector Graphic7.4.1.0 Scanned7.4.1.1.1 Scanned7.4.1.1.4(a) Scanned7.4.1.1.4(b) Scanned7.4.1.1.5 Scanned7.4.1.1.6 Vector Graphic7.4.2.0 Scanned7.4.2.1.4 Scanned7.4.2.1.6 Vector Graphic7.5.1.1.6(a) Vector Graphic7.5.1.1.6(b) Vector Graphic7.5.1.1.6(c) Vector Graphic7.5.1.1.6(d) Vector Graphic7.5.1.1.6(e) Vector Graphic7.5.1.1.6(f) Vector Graphic7.5.1.1.6(g) Vector Graphic7.5.1.1.6(h) Vector Graphic7.5.1.1.6(i) Vector Graphic7.5.1.1.6(j) Vector Graphic7.5.1.1.6(k) Vector Graphic7.5.1.1.6(l) Vector Graphic7.5.2.1.6(a) Vector Graphic7.5.2.1.6(b) Vector Graphic7.5.2.1.6(c) Vector Graphic7.5.2.1.6(d) Vector Graphic7.5.2.1.6(e) Vector Graphic7.5.2.1.6(f) Vector Graphic7.5.2.1.6(g) Vector Graphic7.5.2.1.6(h) Vector Graphic7.5.2.1.6(i) Vector Graphic7.5.2.1.6(j) Vector Graphic8.2.1 Scanned8.2.2.3.1.1(a) Scanned8.2.2.3.1.1(b) Scanned8.2.2.3.1.1(c) Scanned8.2.2.3.2.1 Scanned8.2.2.3.2.2(a) Scanned8.2.2.3.2.2(b) Scanned8.2.2.3.2.2(c) Scanned8.2.2.3.2.2(d) Scanned8.2.2.3.2.2(e) Scanned9.2.3 Scanned9.2.4 Scanned

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MMPDS-0131 January 2003

Figure No. Current Form Figure No. Current Form

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9.2.6 Scanned9.2.11 Scanned9.2.12 Scanned9.2.15(a) Scanned9.2.15(b) Scanned9.3.1.1.2 Scanned9.3.1.1.3(a) Scanned9.3.1.1.3(b) Scanned9.3.1.2 Scanned9.3.1.3 Scanned9.3.1.4(a) Scanned9.3.1.4(b) Scanned9.3.1.5 Scanned9.3.1.6.1 Scanned9.3.1.6.2 Vector Graphic9.3.2.3(a) Scanned9.3.2.3(b) Scanned9.3.2.3(c) Vector Graphic9.3.2.4 Scanned9.3.2.5(a) Scanned9.3.2.5(b) Vector Graphic9.3.2.5(c) Vector Graphic9.3.2.5(d) Vector Graphic9.3.2.7(a) Scanned9.3.2.7(b) Scanned9.3.2.7(c) Scanned9.3.4.1(a) Scanned9.3.4.1(b) Scanned9.3.4.1(c) Scanned9.3.4.1(d) Scanned9.3.4.3 Scanned9.3.4.4 Scanned9.3.4.5 Scanned9.3.4.7 Scanned9.3.4.10(a) Scanned9.3.4.10(b) Scanned9.3.4.10(c) Scanned9.3.4.12(a) Scanned9.3.4.12(b) Scanned9.3.4.13 Scanned9.3.4.16(a) Scanned9.3.4.17(a) Scanned9.3.4.17(b) Scanned9.3.4.17(c) Scanned9.3.4.17(d) Scanned9.3.4.17(e) Scanned9.3.4.17(f) Scanned9.3.4.17(g) Scanned9.3.4.17(h) Scanned

9.3.5.1(a) Scanned9.3.5.1(b) Scanned9.3.5.2 Scanned9.3.5.6 Scanned9.3.6.2 Scanned9.3.6.7 Scanned9.3.6.8(a) Scanned9.3.6.8(b) Scanned9.3.6.8(c) Scanned9.3.6.8(d) Scanned9.4.1.3 Scanned9.4.1.3.4(a) Scanned9.4.1.3.4(b) Scanned9.4.1.3.4(c) Scanned9.4.1.3.4(d) Scanned9.4.1.3.4(e) Scanned9.4.1.5.2(a) Scanned9.4.1.5.2(b) Scanned9.4.1.5.2(c) Scanned9.4.1.5.2(d) Scanned9.4.1.5.2(e) Scanned9.4.1.5.2(f) Scanned9.4.1.5.2(g) Scanned9.4.1.5.2(h) Scanned9.4.1.5.3 Scanned9.4.1.6 Scanned9.4.1.7.2 Scanned9.4.1.7.2, cont. Scanned9.4.2.2 Scanned9.4.2.3.2 Scanned9.4.2.3.5(a) Scanned9.4.2.3.5(b) Scanned9.4.2.5.2 Scanned9.4.2.5.3 Scanned9.5.1.3 Scanned9.5.1.5.1(a) Scanned9.5.1.5.1(b) Scanned9.5.1.5.1(c) Scanned9.5.1.5.3 Scanned9.6.3 ScannedA.1 Scanned