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    _ _

    O K R I D G ~ I O N L L BOR TORYoperated y

    UNION C RBIDE CORPOR TIONfor the

    U.S. TOMIC ENERGY COMMISSION .. A1 //ORN T 333 4

    AN IBM 7090 FORTRAN PROGRAM FOR ASME UNFIRED PRE SSUREVE SSEL E SIGN AND PRELIMI NARY CO ST ESTIMATION

    C. E PrinceR P. Milford

    NOTI EThis document contains information of a preliminary nature and was preparedprimarily for internal use at the Oak Ridge National Laborotory. t is subjectto revision or correction and therefore does not represent a final report. Theinformation is not to be abstracted repri nted or other wi se gi ven publ ic di s-semination without the approval of the ORNL patent branch Legal and Infor.motion Control Department.

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    - - - - - - -- - - - - - - -- - - - - - -- - - - - - -LEG AL NO TICE - - - - - - -- - - - - - -- - - - - - - -- - - - - -This report was prepared as an occount of Government sponsored work. Neither the United States lnor the Commission, nor any person acting on behalf of the Commission:A. a k ~ u any warranty or representation, expressed or implied, with respect to the accuracy,

    completeness, or usefulness of the informotion contained in this report, or that the se ofany information. apparatus, method or process disclosed in this repott may not infringeprivately owned rights or

    B. Assumes any liabilities with respect to the use of, or for damages resuiting from the use ofany tnformation, apparatus, method, or proc.S$ disclosed in this repart.

    As used in the above, person acting on behalf of the Commission indudes any employee orcontractor of the Commission, or employee of such controctor, to the extent that such employeeor contractor of the Commission, or employee of such contractor prepares, disseminates, orprovides access any information pursuant to his employment or contract with the Commission,or his employment with such contractor.

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    ORNL TM

    CHEMIC L TECHNOLOGY DIVISION

    N IBM 7 9 FORTR N PROGR M FOR SME UNFIRED PRESSUREVESSEL DESIGN ND PRELIMIN RY COST ESTIM TION

    C E PrinceR P. Milford

    D TE ISSUED

    OCT 7 962

    O K RIDGE N TION L L BOR TORYOak Ridge Tennesseeoperated by

    UNION C RBIDE CORPOR TIONfor theU S TOMIC ENERGY COMMISSION

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    CONTENTSPage

    Abstract 1Introduction 1Design Equations and Calculation Techniques 1

    Internal Pressure 4External Pressure 4Jacket Design 6

    Limitations and Assumptions 8Outside Diameter Range 8Metal Thicknesses 8Freeboard Ratio Variation 8straight Side Length/ood. Range 9Modulus of Elas t ic i ty 9Head Dimension Approximations 9External Pressure-Thickness Check 10

    References 11Appendix A, Graph for Inside-Depth-of-Dish EquationDevelopment 12Appendix B, List of Variables Used in Calculations 13Appendix C, Program Flow Diagram Sheets 1 through 7 16Appendix D, Listing of Fortran Deck 23Appendix E, Sample Input Data Sheets 1 and 2 33Appendix F Deck Setup for Central Data ProcessingFacility, ORGDP 35Appendix G, Input Data Sheet No. 2 Vessel and JacketDesign and Output Sheets for Sample Problem 36

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    1

    AN IBM 7090 FORTRAN PROGRAM FOR AS:ME UNFIRED PRESSUREVESSEL DESIGN AND PRELIMINARY COST ESTIMATIONC E Prince.R, p, Milford

    ABSTR.I\crI.An IBN 7090 Fort.ran program was wri t ten for the pre l im-

    inary and cost est imation of unfired. pressure vesse lswith or without a jacket Both vessel and jacket designsconform to the 1959 ASME Boiler and Pressure Vessel Code)

    e ~ t i o n VIII) Unfi.red Pressure Vessels. Vessels and jacketsfrom in . pipe through 84 in . o.d., and. 1/4 in . through 1-1/2in . in metal thickness may be designed by th i s program aswri t ten Total vesse l cos t is the sum of metal and f abr ica-t ion costs) each on a weight bas is

    INTRODUCTIONTb e design of an unfired. pressure vesse l under external pressure

    using the ASME Code i s a t r i a l and er ror process involving severa l ca l -cula t ions and the use of charts . This process can become tedious andtLm e 'consuming i f severa l vesse ls a re to be designed.. 1 he increaSing' : tvailabil i y a.nd use of modern h:igh speed computing machines have re -d:ueed the time and e f f o r t requi red for pro'blems of a s imi lar nature toa minimum. With th i s in mind) a Fort.ran program was wri t ten for usewith the IBM 7090 computer which wil l make the necessary design andcost est imat ion calculat ions for these vessels .

    DESIGN EQUATIONS AND CALCULATION TECHNIQUEST he calculat ions in th i s program are eonsi . s tentwi h the rules se tfor th in the 1959 edi t ion of the AS:ME Boiler and Pressure Vessel Code)

    sect ion VIII) U:c.fi.red Pressure Vessels) for the calcula t ion o f wall andhead. thickneps of th in sb.elled. vesse ls subjected to in te rna l or exter -nal preseur'e. Schematic d.iagrams in Figo 1 ana. Fig . ? show the typevessels th i s p:rogramwtll d.esign.

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    Inside DishDepthi

    Inside4 Diameter . I

    Head SphericalDish Radius

    OutsideDiameter

    KnuckleRadius

    Shell

    t

    UNCL SSIFIEDORNL LR DWG 71766

    StraightSidele th

    DesignLength

    1/3 Head Dish Depth

    Fig. 1. Vessel with straight side/outside diameter ratio equal to or less than 4 0

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    3

    UNCLASSIFIEDORNL-LR-DWG 71767

    1/3 Head Dish Depth

    4 x Outside Diameter

    4 x Outside Diameter

    Stiffening Ring

    Note: For long vessels, stiffening rings are required every 4 x OD in.

    Fig. 2. Vessel with straight side/outside diameter ratio greater than 4.0

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    Internal PressureFrom Ref. 1), par. UA-l 1), the equation used for determining the

    shell thickness was:P Ro

    E 0, 4 P ,\'ihere

    t minimum required thickness of shell plates, exclusive ofcorrosion allowance,

    P design pressure, pounds per square inch,Ro8

    E

    outside radius of shel l course,maximum allowable st ress value, pounds per square inch,efficiency of longitudinal welded joints Par. DW-12).seamless shells; use E l.o. )

    (1)

    For

    From Par. u8-4 d), the equation for calculating the head thicknessof an A ME type tor ispherical) head ,vas:

    t

    where

    8,

    t minimum required thickness of head f ter forming, inchesexclusive of corrosion allowance),

    P design pressure, pounds per square inch,L inside spherical head radius, inches}r = inside knuckle radius, inches,E same as in Equation 1) .

    Extp rnal Pressure

    2)

    The charts in Appendix V of Ref. 1) show the relationship of rat ioof the compressive s tress to tangent modulus of el s t ic i ty 8/E) to thed.imensional rat ios of length to outside diameter LID) and thickness toQu.+,eide diameter t iD), The l t ter two are properties which depend uponthe geometry of the system and are the same for l l materials . The

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    5 -

    portion of the chart in the range of this study l ies between the LIratios of 0.8 and 4.0. Vessels in this area are below the cri t icallength and fai lure takes place a t thebe constant. These curves can be

    stress which is assumed toby the following equation,

    Ref. 2):s

    \]here

    1 . 30 tiD) L 5LI - 0.45 t/D)0.5

    t minimum required shell thickness in inches, exclusive of corrosion allowance,S compressive stress, psi,

    E tangent modulus of elast ic i ty and must be essential ly constantthroughout the range in question,

    D outside diameter, inches,L design length of a vessel section, taken as the largest of the

    following:1) the distance between head bend l ines plus 1/3 of the

    depth of each head i f there are no st i ffening rings;2) i f st i ffening rings are required, the design length was

    taken as four times the outside diameter. Neither thecenter-to-center distance between any two adjacentst i ffening rings nor the distance from the center of thef i r s t st i ffening ring to the head-bend l ine plus 1 3 thedepth of the head may exceed this distance. All measurements are taken paral le l to the axis of the vessel, ininches.

    Also shown on the chart are thethe material i t se l f These may be

    tha t are dependent uponby the equation, Ref.

    2) :4

    where

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    5 )ofto

    and

    S, E, D and t are the same as in the above geometry dependentformula (EQuation 3), and

    p maximum allowable working pressure (includes4), psi

    factor of

    The thicknesses of ASME type heads are calculated from eQuationsand 6) EQuation (5) was developed from the charts in Appendix V

    ReL 1) and eQuation 6) from the same reference and i t s similar i tyequation 4), Ref. 1) :

    6)

    whereS, E, and P are the same as in eQuation 4),

    inside spherical radius of the head,th minimum head thickness, exclusive of corrosion allowance,in inches 0To d.etermine the reQuired shel l or head thickness for a given set

    of conditions, S/E values are calculated with a thickness of1/64 in. and increasing the thickness by 1/64 in. unt i l the S/E value,based on the geometry of the system, exceeds thepressure of the system.Jacket Design

    rhis program will design two types of vessel

    value based on the

    They areshown in Fig. 3, The f i r s t type covers l l or part of the straightside portion of the vessel but not the head. The second type coversl l or part of the straight side portion of the vessel and the head of

    the vessel with an ASME type head. Jacket calculations are theSEl me as for the vessel. Connection of the jacket to the vessel on theend opposite the ASME head and on both ends of a side jacket

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    7

    Straight Sidelength

    UNCLASSI FI EDORNL LR OWG 71768

    Notes: 1) Jacket may extend any length along vessel straightside length.2) Stiffening rings on jacket are located 4 x jacket

    apart.

    Fig. 3. Jacket types.

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    is accomplished by -welding to a -washer type r ing The thickness ofthis r ing is taken as t-wice the jacket shel l thickness. Ho-wever, alo\rer l imit of 0, in. and an upper l imit of LO in. vJere assigned toth is thickness.

    A program flo-w diagram is given in Appendix C and a program cardl i s t ing in Appendix D. Sample data sheets and deck setup are given 1nAppendices E and F, respectively. A sample problem sho-wing input andoutput is in Appendix G

    LIMITATIONS AND S S U ~ W T I O N SOutside Diameter Range

    The range of vessel outside diameters i s from 5.563 inches 5 in.NPS Sch. 4 pipe) through 84 inches. These diameters are supplied as al i s t in the second data card. Jacket outside diameters for the type-with one head are also taken from this l : s t . A jacket on the s traightside of the vessel only does not have to match a head and therefore snot res tr ic ted.Metal Thicknesses

    After the addit ion of corrosion allo-wance, the f inal thickness ischosen as the next greater slze from an internal l i s t of standard thj_ck-

    . e s s e s supplied in the third data card. Ho-wever, provision is includedfor accepting the f i rs t standard thickness under the required size i fthe excess is not greater than a certain fraction of tha t standardthickness. This allo-wable excess may be included in the input data asa decimal fraction of the standard thickness. The above feature is notincluded for the four pipe sizes. Their thickness is based on Sch. 4pipe size and the abi l i ty of that thickness to viithstand the designpressures. Corrosion allo-wance is not considered for the foursizes.Freeboard Ratio VariationThe in i t i a l volume estimated is based on a l i s t of internal diameters input data card No 1); each i .d . is sl ight ly less than thecorresponding o.d. in the o.d. l i s t . After an i .d . i s selected -whichmeets the volume requirement, the next larger oed, is selected for thevessel. This -will increase the freeboard rat io s l igh t ly above i t s in -put value.

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    -9straight Side Length/o.d. Range

    This length/outside diameter rat io -was taken as 0.8 to 4.0 becauseone equation could be used to represent the l ine obtained by plott inglength/outside diameter versus stress/modulus of elas t ic i ty for a givendiameter/thickness ratio . For length/diameter rat ios larger than 4.0,st i f fening rings must be used every four diameters distance along theside of the vessel or jacket.Modulus of Elas t ic i ty

    This program is l imited to the range in -which the modulus ofelast ic i ty can be considered constant.Head Dimension Approximations

    Several approximations -were used to obtain values of various headdimensions. Three of these yalues--the head dish volume, the head dishradius and the head knuckle radius--are printed as output and can be

    compared to manufacturer s l i te ra ture The inside depth of dishof the head--not printed as output---was estimated from the equation,y 0.1545 X +1.4158,-which -was obtained by plott ing the inside dish depths versus outsidediameter and dra-wing a s traight l ine through the f ield obtained. Thisdevelopment is sho-wn in Fig. 4, Appendix A. Data Were taken from the1955 Lukens Spun Heads Data book. Calculated head dimensions should becompared 'with manufacturer 's l i terature and the jacket head depth ofdish should be compared to the vessel head to ensure a correct f i tHead dish volume and weight will also vary due to the equations usedfor estimating these values. The head dish volume was estimated fromthe following equation:v ' (0.64) 1. d. 3v = volume in U S gallons,i d = inside diameter in inches,0.64 constant obtained by averaging eight selected heads using data

    from Buffalo Tank Corporation, Ref. (5)The head -w eights were estimated from equations obtained on p. 32 of( 4) .

    8)

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    -10-

    All pipe cap dimensions used Were taken from Ref. 3) and representstandard type caps rather than ASME tor ispherical caps. ThisWill result in a conservative estimate of required thickness of about

    based on calculations a 12-in. pipe cap and a 12-in. dishedhead) ,External Pressure-Thickness Check

    t is possible to check the thickness required by the externalpressure on the or shel l and head by a rapid hand cal -culation using the charts in Appendix V of Ref. 1). The safe Workingpressure may be calculated the thickness determined by the programand compared to the pressure. This is recommended for any designas a f inal since the metal property-dependent l ines in the externalpressure charts of Ref. 1) deviate rapidly from s traight l ines for highL/o.d. rat ios and o.d rat ios belo W 100.

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    -11-

    REFERENCES

    1. "Unfired Pressure Vessels, Section VII, t ASME Boiler and PressureVespel Code, 1959 Edition, Am. Soco Mech. Engr., New York (1959).

    2. E. O. Bergman, It rhe Ne-w-Type Code Chart for the Design of VesselsUnder External Pressure, Pressure Vessel and Piping Design, collected papers 1927-1959, p 649, Am. Soc. Mech. Engr., Ne-w YorK.

    3. Tube-Turn Catalog and Engineering Data Book, Number 211, TubeTurns, Inc., Louisville 1, Kentucky 1949) 4. Lukens Steel Company Spun Heads Catalog, 1955, Lukens Steel Com

    pany, Coatesville, Pennsylvania (1955).

    5 Buffalo Tank Handbook, 5th Printing, Buffalo Tank Company, Ne-wYork (1945).

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    UNCLASSIFIED16

    Appendix A

    14 ~./12C

    c0=- 10cV'la Notes: (1) , Doto from Lukens Spun

    0 Heads, Doto Book, 1955,c a pp. 33-39.(2) A Tube Turn, Doto BookIl IU0 211, and are not ASME di - f-JU mensions I\Q (3) Formula: IDD (0. 1545} Iin OD + 1.1458.6Q< :c

    41 / :t / ;3. o 8 16 24 32 40 48 56 64 72 80 88 96

    OUTSI DE DIAMETER (OD), in.

    Fig- 4 Data for head inside depth of ish equation development .

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    Variable NameAAl, AA5 A6, A7A8 A9A5J, A6J, A7JBlCMYCFPPCMPPCMPPJCORCOSTBCOSTMCOSTMJDENSDENSJDENSQDENSQJDIDIHDIJDISO

    DOJ

    DOJEPEEJFBRHHSEPCHSEPCJ

    -13-

    APPENDIX BList of Variables Used in Calculations

    VariableUsed to float indexWorking value of thickness, in.Used to input material of constructionof vesselVessel ident if icat ionUsed to input jacket material of con-structionWorking value of head thickness, in.Working value of shell thickness, in.Design capacity, cu tCost of fabrication, / lbCost of vessel metal, / lbCost of jacket metal, / lbCorrosion allowance, in.Cost to fabricateCost of vessel metal,Cost of jacketVessel metal density, lb/cu tJacket metal density, lb/cu tVessel metal density, lb/cu in.Jacket metal density, lb/cu in.Working value of vessel shell insidediameter, in.Inside diameter of head, in.Inside diameter of jacket shell , in.Final vessel shell inside diameter, in.Working and f inal vessel outside dia-meter, in.Jacket outside diameter (working valueunder internal pressure and finalvalue), in.Jacket outside diameter (working valueunder external pressure), in.Vessel metal modulus of psiJacket metal modulus of psiFreeboard ratio, (vessel volume/designvolume)Vessel shell length, in.Unsupported vessel shell length used inrequired thickness calculation, in.Unsupported jacket shell length used inrequired thickness calculation, in .

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    APPENDIX B (continued)Variable Name

    IJJHEDJLO )K, L L1 L2PEXPEXJPINPINJQl, Q2, Q3, Q4RADHRADHJR DKRADKJRK2, RK3RK2J, RK3JBLODSSJSEGHSEGHJSEGSSEGSJSEPHSEPHJSEPSSEPSJSFBPACESSLSSLJSSLRJTCOSTTCOS I B

    ~ C O S T MTCOSTITEIEPJTEMP

    VariableIndex or integer valueInput - i f vessel is to have a jacket,this variable is oneInput - i f jacket has a head, this var ible is oneInternal equivalent of a sense switch,set i f jacket L/o.d. is greater than 4Index valueDesign external pressure for vessel, psiDesign external pressure for jacket, psiDesign internal pressure for vessel,Design internal pressure for jacket, psiWorking values used in average calcula-tions (see 41, 486Vessel head spherical dish radius, in.Jacket head spherical dish radius, in.Vessel head knuckle radius, in.Jacket head knuckle radius, in.Working values vessel knuckle radius, in.Working values jacket knuckle radius, in.Vessel s traight side length/outside dia-meterMaximum allowable s tress in vessel metal,psiMaximum allowable s tress in jacket metal,

    psiS/E due to geometry of head, vesselS/E due to geometry of head, jacketS/E due to geometry of shel l , vesselS/E due to geometry of shell , jacketS/E due to pressure on head, vesselS/E due to pressure on head, jacketS/E due to pressure on shel l , vesselS/E due to pressure on shell , JacketLength of head s traight flange, in .Min. space between jacket i d and ves-sel o.d., in.Vessel straight side length, in.Jacket straight side length, in.SSLJ/SSLCost of vessel only (metal fabrica-tion), :I;Total fabrication cost, :I;Total metal cost, :I;Total unit cost, :I;Thickness of end plate, in.Design temperature for vessel, of

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    APPENDIX B continued)Variable Name

    T MPJTH

    THC.rHCASTTHEPTHEPJTHIPTHIPJTHJTS, TSC, TSCAST,TSEP, TSEPJ, TSIP,TSIPJ, TSJTSEPJITWJTWJV

    TWVVOHVOLHTTVTlVT2WEL

    WELDJWJEWJHWJSWTHWTSWTSRWTSRJXSIJ: A

    VariableDesign temperature for jacket, ofVessel head thickness no corrosion a l-lowance), in.Vessel head. thickness plus corrosionallowance, in.Vessel head thickness plus corrosionallowance as standard thickness, in.Vessel head thickness due to externalpressure, inJacket head thickness due to externalpressure, in.Vessel head thickness due to internal

    pressure, in.Jacket head thickness due to internalpressure, in.Final jacket headThe followingcounterparts ofthickness, in .variable are shellabove head values

    Jacket - Sch. 40 NPS thickness, in.Weight of jacket, IbsTotal weight of uni t vessel plus jacket),IbsWeight of IbsVolume of one head dish, galVolume of two caps not includingstraight ), cu f tTotal volume of cu f tFi rs t estimate of to ta l volume of ves-sel, cu f tRatio of VTl VTWeld efficiency, ves decimal frac-t ionWeld efficiency, jacket, decimal frac-t ionWeight of one end, IbsWeight of one jacket head, IbsWeight of jacket IbsWeight of one vessel head, IbsWeight of vessel IbsDistance from head weld to f i r s t s t i f fening ring, yes in.Distance from head weld to f i r s t s t i f fen-ing ring, jacket, in.Excess thickness allowable above astandard size before requiringthe next standard thickness,expressed as a decimal fraction ofthe standard size

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    12,100,200

    Set Length ofShell forCalculations

    Yes

    Yes

    203 Set Head Radi usThickness, Volume

    AFortran Statement Number

    -16-

    InputDiameters and Thicknesses

    Calculate Vessel Volume,I. D. and Requ ired O. D.

    Is No

    UNCLASSI I EDORNL-LR-DWG 71758

    Length/O.D. >----------->4

    2026

    Set Length ofShell forCal cu lations

    No< 10.75 :>------...

    208

    SHEET 1 OF 7APPENDIX C

    PROGRAM FLOW DIAGRAM

    Calculate ShellThickness dueto ExternalPressure

    B

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    A

    2 Calculate ShellTh ickness under

    Requ ired Externa IPressure

    IsPipe Shell

    Thick Enoughunder External

    NoPrint:

    OutputFormalGo To

    I nput Data\0)

    Print:OutputFormat

    Go ToInput Data

    10)

    Yes

    -17-

    No

    306

    Yes 320

    No

    CSHEET 2 OF 7

    B

    Shell Thicknessdue to External

    Pressure

    UNClASSI FI EDORNl-lR-DWG 71759

    DoesThickness ExceedInternal list Range

    Pri nt:Shell Thickness Too

    Small

    Determine HeadSpherical Radiusof Selected

    Calculate HeadThickness due toExternal Pressure

    DoesThickness Exceed

    Internal list Range

    Print:Head Thickness Toe

    Small

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    404

    Yes

    Go ToInput Data10)

    4 6

    -18-

    C

    400Thickness due

    to Internal Pressure

    4001 r s;t. Head Knuckle

    4 3 Calculate Head

    Yes

    Does ShellThickness ExceedSch 40 Pipe

    Thickness due toInternal r e s s u ~

    Thickness Lessthan Shell Thickness

    due to InternalPressure

    No

    405OD 10.75

    No

    Print:

    No

    420No

    Pri nt:

    UNCLASSIFIEDORNL-LR-DWG 71760

    Does InternalPressure ControlShell Thickness

    Yes

    Print:Pipe Thickness

    OKExternal PressureControls Shell

    InternalPressure Controls

    Shell

    DE

    SHEET 3 OF 7

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    Pri nt:RequiredThickness

    Go ToInput Data10)

    490 Set Pipe andCop Size toStd. Sch 40

    Print:Vessel Sch40 Pipe

    DoesHead ThicknessExceed Sch 40Pipe

    Yes 480

    9

    No

    Pri nt:Externa I PressureContra Is Head

    OD 4.0

    590

    No

    JacketDesign?

    Pri nt:

    Yes

    Print:

    UNCLASSIFIEDORNL-LR-DWG 71762

    "Distance BetweenStiffening Rings

    "Jacket for Vesse I

    6 1

    6 1 DoesJacket CoverVessel Head

    63 Shell Thicknessdue to InternalPressure

    635OD < 10.75

    /Set Thi ckness Equalto Sch 4 Pipe; SetHeat Spherical Dish

    No

    Radius

    SHEET 5 OF 7

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    G

    Print:External PressureControls Shell

    613

    H

    Print:Internal PressureControls She II

    Go To 597Clear All Variables

    No

    Print:Required Thickness

    Go To 97Clear All Variables

    Yes

    IsRequ ire d Th i ckness Sch 40 Pipe

    -21-

    Yes

    652

    6 4 1 - - - - - ~ L - - - - - ~Set Shell Length; OD;Calculate Thickness due

    to External Pressure

    IsMin. SpaceRequirement

    Satisfied

    UNCLASSIFIEDORNL-LR-DWG 71763

    No

    Yes

    OD 10.75 No

    Yes

    679

    ~ ~ ~Set Head Spherical. Dish Radius

    Calculate HeadThickness due toInternal Pressure

    JSHEET 6 OF 7

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    No

    Pri nt:RequiredThickness

    Go To 597Clear Variables

    IsShe ~ e ~ ~ ~ e ~ a p

    Sch 40 PipeYes

    -22-

    J680 Calculate HeadThickness due to

    External Pressure

    UNCLASSIFIEDORNL-LR-OWG 71764

    687 Choose Contro II ing

    Yes

    Shell and Head Thicknesses

    720

    7240

    Print:Contro II i ng Pressuresfor Shell and Head

    Go To 597Clear Variables

    Note: Program nds After All Data Has Been Read.

    SH T 7 OF 7

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    UNFIRE PRESSURE VESSEL ESIGN DATA SHEETAPPENDIX EUNCLASSIFIED

    ORNL-LR-DWG 71756

    NRITTEN REQUEST NUMBER DATE (SHEET 1 OF 2)Control Cards:

    5[UT I I I I I I [ I I I I I [ I I I I ITTTTTT I [ I LLLLLL I I I I I I I I I I I I I [ I [ I [ [ [ I [ I [ I [ [ I I I [ I

    1 1 ~ l v l v \ l r l 1 1.lvlvlvl,I,[iJ loluIJ lduLUuLUTTTIOJlLLW] ITTTTTIII ITTTTTTIIIII IIIIII

    NOTESI. ID, SHOULD HAVE JOB DESCRIPTION OR TITLE, NAME, AND ADDRESS.2. CHARGE: 4-DIGIT NUMBER SUPPLIED Y COMPUTER OPERATIONS.3. DUMP, ADDITIONAL TYPES OF DUMP MAY E SPECIFIED.4. TYPE, IF FORTRAN DECK IS TO E RUN, CHANGE BINARY TO FORTRAN.5. SETUP, PLACE THESE CARDS IN FRONT OF BINARY DECK (OR FORTRAN) IN

    THE ABOVE ORDER, FOLLOW WITH DATA CONTROL CARD, THE THREE DATACARDS WHICH CONTAIN THE DIAMETER AND THICKNESS LISTS, AND THEVESSEL DESIGN DATA CARDS.

    II\UJI

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    APPENDIX E ( CONT D)WRITTEN BY,Vessel Doto,

    Capacity,cu It

    Jacket Design Dota:

    Jacket StraightSide/VesselStraight Side

    freeBoardRatio

    Min. Spaceetween

    Vessel OD andJacket 10,

    Materiol ofConstruction

    2)

    NOTES:

    StraightSide/

    OD Ratio

    De,ignExternalPressure,

    psi

    MetalDensity,Ibs/cu ft3)

    UNfiRED PRESSURE VESSEL DESIGN DATA SHEET

    HeadStraightFlange,Modulu.

    in.ofElasticity,

    DesignInternalPressure,

    psi

    MetalDensity,Ibs/cu in.3)

    psi

    DesignTemp.,O

    IREQUEST NUMBER,

    Maximum DesignAllowable Temp.,Tensi Ie, Stress ofpsi 49

    Modulus Maximumof AllowableElasticity, Tensne, Stresspsi psi

    DesignExternalPressure,

    psi

    DATE:

    MetalCost,

    /Ib

    DesignInternalPressure,

    psi

    WeldEff.,Dec.roet

    J

    K

    6

    UNClASSIFI EDORNl-lR-DWG 71757

    3

    4

    l. All decimal paints are coded to the extreme right of the field and do not take up a spoce. However, a decimal point may be located in any other spoce and will override the printed point.(See: Heod-stroight flange in card No.1).

    2. Use any Fortran charac ters.3. Only one density value required.4. The final shell and head thicknesses of the vessel are selected from an internal list by selecting the next larger size. To allow a small overage above one std. thickness before choosing the

    next larger size insert allowable excess as decimal fraction of std. thickness.5. All four dota cards must be included for each vessel.6. J: If Q jacket is to be designed, insert 11'.7. H If 0 iacket is to have a head, insert lit. Jacket may have no more than one head

    I[\+-I

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    APPENDIX DListing of Fortran Deck

    C U ~ F I R E C PRESSURE VESSEL D E S I G ~ P R O G R A ~ , R.P. ~ I L F O R D , C.E. P R I ~ C E 0Oll'ENSICN DIAI(27),DIAOI27),TH[KII4) IIOREACINPUTTAPEIO,2,(CIAlll),INI,27),(oIAOI}I,IIII.27), 2I Tt-'IK(II,IIII,14) 32 F C R ~ A T I 2 7 F 2 . o / 4 F 5 . 3 , 2 3 F 2 . 0 / 1 4 F 4 . 4 ) 4C 9 REAC IN CATA 5IDCREAC INPUT TAPE I C , J I , I C A P y , F B R , R L O D , S F , E , , T E M P , P E X , P I ~ . C M P P , C F P P 61 , ~ E L C , C C R , X S T A . A 5 , A 6 , A 7 , A 8 , A 9 , 0 E ~ S , D E N S C , S S L R J , S P A C E , J H E D , P E X J , P I N 7

    2 J , T E ~ P J , E J . S J , C M P P J , ~ E L C J , J , A 5 J , A 6 J , A 7 J , O E N S J , O E N S C J I 8IICFCRPAT(FIC.D.F5.0,FB.D,F5.0,EID.D,FIC.O,F6.0,F8.o,F 8 01 9IF8.C.F8.0.F4.O,F5.0,F5.C.3A6,2A4,F8.C.F8.0/FB.O,FB.0.11 ,F7.0 ,F7.0, 102 F 6 . [ . E I 8 . o , F 9 . C , F 8 ~ 0 , F 4 . n , I l / j A 6 , F 8 . 0 , F 8 . 0 1 IIC 12 CALCULATE VESSEL VOU.:ME 12VT/ICAPY-FBR 13C 99 SELECT INSLOE DIAMETER FOR REQUIRED VCLUME 14ICn OC1991111,27 15DII/CtAI II 16

    SSL#CI*RLOD 17VT J I 3.14 I59 *0 1** 2*$ SLI I 172 B. *4. ) + I .2 B D} 3 1 I 728. * 7 481 ) 1BIFIVT-VTIIICI,IC2,IC3 1910IOIl/DIAIII-I) 20IC2 GCTC20C 21IC3 VT2/1VTl/VT 22IF(VT2-C.97) 199,2CC,20C 23199 C O N T I ~ U E 24CI990 SELECT ~ E X T GREATER S T A ~ O A R C OUTSIDE DIAMETER 25200 002011111,27 26DOIICIAC I) 27IF(CO-CI)201,202,2C2 28201 CONT INUE 29C2010 SET LFNGTH Of SIDE FOR lSE IN CALCULATIONS 30202 SSLIICC*RLOC 312020 HIISSL-3. 322C21 IFIRLOC-4.12022,2C22,2024 332022 HSFPCIISSL+2.*(.1545*CO+I.14581/3. 342023 Gt T 2026 352024 H ~ E P C I / 4 . * D O 362025 WTSRUHSEPC-I.5-1.1545*CC+I.14SEI/3. 372026 IFICO-IC.751203,207,208 38C2027 IF VESSEL IS PIPE, SET SHELL T H I C K ~ E S S EQUAL T SCHEDULE 40 PIPE, 39C2C28 ALSC SET HEAD CISH RADLlS A ~ C VCLUME. 4n203 IFICO-6.6251204,205,206 412[14 TSEP#THIKlll 42RACb#4.42 43

    V C U I / . ~ 2 . 8 / 1 7 2 8 . 44RACK .A4 45GCTC211 46205 TSEP#TrIKI21 47RAOr#5.31 48VCLrN67.8/1728. 49KACKIII.OJ 50GOTC211 51206 TSEPI/THIKI31 52R4C 1I6.98 53VCLrNI47./1728. 54RACKNI.j3 55GOTC2 I I 56207 T S E P ~ T H I K ( 4 ) 57RACr1/8.77 58VCLr#354.8/1728. 59

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    APPENDIX D (continued)

    RACK III .67 60C 210 CALCULATE S E VALUES BASED ON GEOMETRY OF SYSTEM AND PRESSURE TO 61C21CO SEE iF SCH 4C PIPE IS ThiCK ENOUGH lNDER EXTERNAL PRESSURE 6221 I DC 2115 ltII,96 63AI#I 64AIIIAI*.015625 65SEGSIII.3*{AI/D01**1.5/(HSEPC/DO-.45*SQRTFIAI/D01) 66SFPSI/2.*PEX*DOIIE"Al) 67I FI S EGS- S EP S ) 2 I I 5, 2 I I 6, 2 I 16 682115CCII

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    APPENDIX D (continued)

    308IFICO-24.)312,311,309 1203Q9 IF ( CO- 30. ) 3 J 3,3 1 J ,31 C 12 J310 IFICO-36.l313,311,313 122311 RACI-' CC 123G C T C ~ 2 0 124312 IF(CO-16.1313,314,313 125313 RADI-'I/CC-2.D 126GCTC32[, 121314 RACl-'liDO-I. 0 128GOTC 320 129315 RACHI/CC-6.0 130GCTC320 131316IF(CO-84.1311,311,311 132

    311IF lSEP-0 .513 I ) ,3 l1d l f l 133318 RACH#CO-6.0 134C 319 CALCULATE HEAD TnLCKNESS FOR VESSEL D L A ~ E T E R S LARGER T H A ~ 135C3190 10 IN. PIPE UNCER EXTERNAL PRESSURE 136320 DO 323 1 1,96 131TI-'FP#I 138THFPliTnEP*.CI5625 139SEGrI/0.12*THEP/RADH 1403221 SEPI-'#2.*PEX*RADH/IE*THEPI 1413222 IFISEGH-SEPI-'13223,324,324 1423223 IFII-96)323,3224,3224 1433224 WRITE OUTPUT TAPE 9,3225,A8,A9 1443225 F O R ~ A T JHI,5X40HHEAC 1HICKNESS TCO S ~ A L L FOR VESSEL NO. 2A4) 145323 CCNTLNUE 146324 IFITHEP-TSEP)325,400.40[ 141325 THEPIHSEP 148C 399 CALCULATE THLCKNESS OF SHELL UNDER INTERNAL PRESSURE ALL O I A ~ E T E R S 149400 TSIP/iIPIN*DC/2.I/IS*hELC+.4*PINl 150C400+ E S T I ~ A T F HEAD KNUCKLE RADIUS BASED CCNTROLLING TI-'ICKNESS 151IF{CC-II.14C3,403.4CCO 1524000 RK2/i.06*DO 153

    4001 IF(lSEP-TSIP)4C04,4D02.4002 1544002 B611TSEP 15540C3 GC TO 4005 1564004 B6ltTSIP 1514[05 RK3li3.*B6 158IFtRK2-RK3)4D2.401.4CI 159401 RACKI/RK2 160GOTC4[3 161402 RACKNRK3 162C4029 CALCULATE HEAD THLCKNESS DuE TO INTERNAL PRESSURE 1634C) THLP PIN-RACH*C.25*(3.+SQRTF(RADH/RACK)11/12.*S*WELC-.2*PINI 164IFITHIP-TSIP)404,405,4(5 165404 THIPtiTSIP 166405 IF(CC-IC.15J406,406.420 161C4058 C C ~ P A R E REQUIRED S ~ E L L ND HEAD THICKNESS TO SCH 40 PIPE FOR 168C4[59 DlAfJETERS EQUAL TO OR LESS THAN 10 11'1. PIPE 1694[6 IFtTSIP-TSEPI401.401,qOe 110qC1 TS/iTSEP 1114010 WRLTECUTPUTTAPE9,4011 112

    4 0 1 I C F C R ~ A T I IHI.5X10HSCHECULE 40 P(PE SHELL THICK ENCUGH FOR INTERNAL A 113INC EXTERNAL PRESSURE I 4GOTC4C9 115408 WRITECUTPUTTAPE9.4C8C 1164 0 8 0 C F O R ~ A T I H J . 5 X 5 6 H S C H E C U L E 40 PIPE roo THIN FOR REQUIRED INTERNAL PR 111I ESSUREI I l 118q08J WRITE OUTPUT TAPE 9.4082.TSIP 179

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    PPENDIX continued)

    40820FCR/IATIIH ,4X24HRECUIREC Si-IELL Ti-ILCKNESS F 30 .4 /1 l 180GCTC214 IA I

    4C9IFITHIP-THEP14IC,41C,411 182410 TH#THEP 183

    41Cn WRITECUTPUTTAPE9.4JOI IB44ICICFOR,...ATI1H ,SX68HSCHECULE 40 PIPE CAP THICK ENOUGH FeR INTERNAL AND 185I EXTERNAL PRESSLRE I I 86

    GCTC4HC 187411 WRlTEOUTPUTTAPE9.412 1884120FOR,...ATlIHI,SX6CHSCHEDULE 40 PIPE CAP TOC THIN FOR R E ~ U I R E D INTERNA 189

    IL PRESSURE/II} 190412 W R I T E C U T P U T T A P E 9 , 4 1 2 1 , T ~ I P 1914121 FOR,...Af IH ,5X23HRECUIREC HEAC THLCKNESS24XF7.4} 192

    GOT0214 193C4198 CHOCSE CCNTROLLING THLCKNESS OF SHELL A ~ D HEAD FOR DIAMETERS 194C4199 GREATER THAN 10 IN PIPE 195

    420 IF (TS IP -TSEP142 I ,42 I ,422 19642 J TSIITSEP 197

    4210 WRlTEOUTPUTTAPE9,4211 1984211 FORf'AT( IHI.SX47HSHELL THICKtl.ESS CONTROLLED BY EXTERII.AL PRESSURE/} 199

    GOTC423 200422 TSIITSIP 2014220 WRITEOUTPUTTAPE9.4221 202

    4221 FOR,...ATI IHI,SX47HSHELL THICKNESS CONTROLLED BY INTERNAL PRESSLREI} 203423 IF(THIP-THEP}424,424,425 204424 THNTHEP 2054240 WRITECUTPUTTAPE9,4241 206

    4241 FORf'ATlIH .5X46HHEAD THICKNESS CONTRCLLED 8Y EXTERNAL PRESSURE/I} 207GCTC480 208

    425 THIITHIP 2094250 W R I T E O U T P U T T A P E 9 . 4 2 ~ 1 2104251 FOR/IATIIH ,5X46HHEAD THICKNESE CONTROLLED :IY INTERNAL PRESSURE/I} 211

    480 IF(CO-IO.7S149C,490,48CC 212C 4 8 C ~ ACC CORROSICN ALLOWANCE TO VESSELS OF GREATER THAN 10 IN . PIPE 213

    4800 TSCNTS+COR 214THC#TH+CDR 215

    C48C2 SELECT NEXT LARGER STANDARD THICKNESS OVER REQUIRED THICKNESS FOR 216C4083 B O T ~ SHELL AND HEAO 217

    DC48 j I#5 ,14 216IF ITSC-THIK (L ) }482 .482 ,481 219

    481 Q I# IT SC- T H IK( I ) ) /T H lK ( I I 220Q2I1XSTA*THIK I 1 221

    8 LFIC2-(J)1482I ,482,482 222482 TSCASTI lTHIK( l l 223

    GOT0485 2244821 IF( I -1414B,,1 I822,1 I822 2254822 TSCAST#TSC 226

    483 C C ~ T I N U E 7271185 D0488INS,14 228IF THC-THLKIL1)487,487,486 229

    486 Q3#( f I - 'C-THIK( I l I IT I - ' IK( l l 230QI,IiXSTA"THIK(11 231

    4861 IF(C4-C3}4871,481.1 I87 232487 THCAST#THLK(I} 233

    GCTC500 2344871 IF ( I -1414S8,4872,4872 2354872 THCASTNTHC 236

    488 CCtl.TINUE 237GOT0500 238490 TSCASTNTS 239

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    APPENDIX D continued)THCASHTH 24049Cl WRITE OUTPUT TAPE 9,4902 241

    4 9 0 2 o F O R ~ A T ( IH ,4Xl04HBASIS CF ANSWER IS SCH 40 PIPE wITH CORROSICN ALL 242I O ~ A ~ C E OF DIFFERENCE BETwEEN RECUIRED ND STC T H [ C K ~ E S S I I ) 243C 499 CALCULATE F1NAL VESSEL V O L U ~ E ND FREEBOARD RATIO 244500 DISNDO-2.*TSCAST 245IFICC-IC.75150I,50I,502 246501 V T R ~ . 1 4 1 5 9 * D t S * S S L / ( 4 . * 1 7 2 8 . ) + V O L ~ 247GCTC503 248502 D I ~ C O - 2 . * T H C A S T 2495020 V T N ~ . 1 4 1 5 9 * C I S * * 2 * S S L / ( 4 . * 1 7 2 8 . ) + 1 . 2 8 * D I H . * 3 / ( 1 7 2 8 . * 7 . 4 8 1 ) 2505C3 FBRIiVTlCAPY 251C503+ CALCULATE WEIGHTS NC COSTS 2525030IF OENS)S031,5031,5C39 2535031 D E N S D E ~ S Q * 1 7 2 8 . 2545039 WTSN3.14159*DENS*H*ICO*CO-OIS*OlS)/ 4.*1728.J 255

    I F ( T H C A S T - I . 1 5 0 4 , 5 0 ~ . 5 [ 5 2565 4 W T H N C E N S * T H C A S T * I D C + O O / 2 4 . + 3 . + 2 . * R A C K / 3 . 1 . * 2 * 3 . 1 4 1 5 9 / 1 1 7 2 8 . * 4 ~ ) 257GCTC506 2585[50WTHNDENS*THCAST*(DO+OO/24.+3.+2.*RADK/3.+THCAST)*.2*3.14IS9/11728. 2591*4.1 260506 TWVNWTS+2.*WTH 261C C S T ~ C ~ P P * T h V 262COSTBNCFPP*TWV 263TCOST#CCSTM+COSTB 264510 IFICC-10.7S)SII.511,512 265511 VOHD VOLH*7.481/2. 266GCTOSI3 267512 VCHCU.64*IDIH/12.J**3 268C5129 WRITE CUT RESULTS 269513CWRITEOUTPUTTAPE 9 , 5 1 4 , A e , A 9 , A S , A 6 . A 7 . T E ~ P , C A P Y . F B R , V T . V C H D . R L O D , D O 270I,TSCASr,H,THCAST,RADH,RADK,SF.WTS,wTH 271

    5 1 4 C F C R ~ A T ( IH ,4XI3HVESSEL NUMBER28X2A4/5X24HMATERIAL CF CONSTRUCTION7 272IX3A6/5XI3HDESIGN TEMP FF37.[IISX2/HOESLGN CAPACITY CU FTF32.3/SXI5 2732HFREEBOARD RATIOF37.2/SX20HVESSEL VCLUME FTF33.3/5X24HONE HEAD 2743 DISH VOLUME GALF28.2/SX29HSTRAIGHT LENGTH IOUTSIDE D I A ~ F 2 4 . 3 / S X 2 0 2754 H O ~ T S I C ~ u[AMETER IN.F34.4/5XI9HSHELL THICKNESS IN.F35.4/5XI6HSHEL 276LENGTH I N . F 3 7 . 3 1 ~ X I 8 H H E A D THICKNESS IN.F36.4/5X2CHHEAC DISH RADI 2776US IN.F33.3/5x23bHEAC K ~ U C K L E RADIUS IN.F3U.3/5X24HbEAD STRAIGHT F 2787LANGE IN.F2e.2/5X/9HwELGHT OF SHELL LBSF34.3/5X22HwEIGHT OF CNE HE 2798AC LRSF31.3) 2BO5IS0wRITEOUTPUTTAPE9,516.TWV.DENS,DENSQ,PEX,PIN,E.S,CCR,XSTA,wELD,CMPP 281I,CFPP,COSTM,COSTe,TCOST 282

    5 1 6 0 F C R ~ A T ( IH .4X26HTOTAL ~ E I G H T OF VESSEL LBS F27.31 5 X 2 6 H ~ E T A L DENS I 283ITY LB PER CU FT F27.31 5X27HMETAL DENSITY LO PER CU IN. F27.41 5X2 2842 8 H D E S I G ~ EXTERNAL PRESSLRE PSI F23. II Sx28HDESIGN INTERNAL PRESSUR 2853E PSI F23.11 5X2SHMCCULLS OF ELASTICITY PSI E34.51 5x32HMAX AlLOwA 2864BLE TENSILE STRESS PSI FI8.CI 5x23HCCRRCSION ALLOWINCE IN. F31.41 28755X35HALLCWANCE OVER STD THIK. DEC.FRACT. F19.41 SX26HWELC EFFICIEN 2886CY CEC.FRACT. F27.311 5 X I 9 H ~ E T A L COST $ PER LB F3S.41 5X25HFABRICA 2897TICN COST $ PER LB F29.41 5XI9HMETAL COST TOTAL $ F34.31 5X25HFAB 2908RICATION COST TCTAl $ F2A.311 5XI8HTOTAL UNIT COST $ F35.3111 2915160 WRITE OUTPUT TAPE 9,5161 292

    5 1 6 I Q F C R ~ A T ( IH ,4X54H(THE AeCVE CALCULATICN IS FOR ASME TORISPHERICAL H 293IEAC)) 294520 IF RLOD-4.1590,590,521 295521 WRITE CUTPUT TAPE 9,52IC,HSEPC,wTSR 296S 2 / 0 C F C R ~ A T I IH ,4X10CHTHE AeCVE RESULTS A S S U ~ E THAT STIFFENING R I ~ G S R 297IE PLACEC NO GREATER THIN 4 OUTSIDE D I A ~ E T E R S APART F7.3,IX 7HINCH 2982ES1I 5X 98HAND ALSO NO FURTHER THAN 4 CUTSIDE DIAMETERS MINUS 1.5 299

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    APPE:fjlJIX D (continued)

    C

    CC

    c

    3 1 /3 ~ E A D lOCI FROM THE HEAD-TO-SHELL kELDI F7.3,IX 7HINCHES)590 IF(J1597,597,6CO597 DO 598 1 15,134598 THIK(IJIJO.599 GC TO ICJACKET DESIGN CALCULATIONS600 WRITE OUTPUT TAPE 9,600C,A8,A96000 F C R ~ A T I IHI,5X2EHJACKET FOR VESSEL N U ~ B E R60CI IF(DENSJ)6002,6CC2,6CI6C02 DFI\SJIIDfNSQJoll28.60IIFIJHED)601I ,6CII ,63CJACKET ON STRAIGHT SIDE Of VESSEL ONLY

    2A4/11l

    60116026C3604

    JACKET SHELL THICKNESS, INTERNAL AND EXTERNAL PRESSLREDIJIIDC+2.oSPACE

    60406041604260436044

    TSIPJII(PLNJ*CIJ/2.J/ISJoWELCJ-.6*PINJJS S L J ~ S S L * S S L R J00 605 1111,96TSEPJIIITSEPJIITSEPJ*.015625DOJIIDIJ+2.*TSEPJIF(SSLJIDOJ-4.)b045,6045,6o44SSLJII4.*OOJHSEPCJIISSLJJLOClilhTSRJIIC.

    6045 SEGSJIII.3*(TSEPJ/CCJI**1.5/ISSlJ/DOJ-.45*SQRTFITSEPJ/OOJ))6C46 SEPSJII2.*PEXJ*DOJ/IEJ*TSEPJI6047 IFISEGSJ-SEPSJ)6C5.6C6,606605 CCf\ TINUE606 IF(TSIPJ-TSEPJI607,607,609607 TSJIiTSEPJ6070 WRITE OUTPUT TAPE 9,608608 F O R ~ A T ( I H ,5X42HEXTERNAL PRESSURE CONTROLLING JACKET SHELL/)GC TO 6 I6C9 TSJIHSIPJ6090 WRLTE OUTPUT TAPE 9,610610 F O R ~ A T I IH ,5X42HINTERNAL PRESSURE CONTROLLING JACKET SHELL/)END THICKNESS611 TEIEPJII2.*TSJIF ( TE I E P .25 )6 I 10, ) I I 0 ,61 I I6110 TEIEPJII.25GO TO 613I FIT E I EPJ- I 16 I 3 , 6 I , 6 1 I 2TEIEPJIII.61 J I6112C WFIGHTS AND COSTS FOR JACKET, AND JACKET PLUS VESSEL613 WJSIIDENSJ*SSLJ*3.14159*IOOJ*OOJ-DIJ*OLJ)/14.*1728.)614 ~ J E D E N S J * T E I E P J * 3 . 1 4 1 5 9 . ( D I J . C I J - D O * C O ) / { 4 . * 1 7 2 8 . )615 TwJNWJS.2.*hJE

    CC

    616 TWJVNTWV+TWJ617 C C S T ~ J I I T W J * C M P P J618 TCOST8HTWJV CFPP619 T C O S T ~ I I C C S T ~ + C C S T M J620 T C O S T I T C O S T ~ + T C O S T ~t2 GC TO 734JACKEf wITH ONE HEADJACKET SHELL THICKNESS CUE TO INTERNAL PRESSURE630 DOHOO

    L l l i631 DO 634 LlIlI,27L2 L

    3003013023033043053063073083093103113123133143153163173183193203213223233243253263273283293303333333334.33533633733339340341.;4234334434534634734834935035135235.1354355356357358359

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    PPENDIX D (continued)632 I F I C C J - C I A O I L 6 ~ 3 6 3 4 6 3 4 360633 DOJNDIACIL 361TSIPJIIIPINJ-COJ/2.)/ISJ-WELCJ+.4-PINJl 362IF( IDCJ-2.-TS[PJ-DO)-12.-SPACEJ )634,641 ,641 363634 CCNTINUE 364C J CKET SHELL T ~ I C K N E S S CUE TO EXTERN L PRESSURE 365641 S S L J ~ S S L - S S L R J 3666410 DCJEPIIDO j67642 DO 649 1111,27 3686420IF(COJEP-CIAO(L6421.649,649 3696421 DCJEPIlDIAOI I) 3706422 HSEPCJIISSLJ+(.1545*DCJEP+I.145el/3. 3716423 IFlhSEPCJ/DCJEP-4.J643,643,6424 3726424 H S E P C J ~ 4 . - D C J E P 373WTSRJllhSEPCJ-I.5-( .1545.DOJEP+I.1458l/3. 374JLCCIII 375643 DO 644 KIiI,96 376TSEPJIIK 377TSEPJIITSEPJ*.015625 378SEGSJIII.3*(TSEPJ/DOJEPl--1.5/IHSEPCJ/DOJEP-.45*SQRTF(TSEPJ/DCJEP 379SEPSJN2.-PEXJ-DOJEP/(EJ-TSEPJ) 380IF(SEGSJ-SEPSJ)644,645,645 381644 CONTINUE 382645 IF( (DCJEP-2.-TSEPJ-DO)-(2.*SPACE) )649.6450,6450 3836450 IFIAPSFICOJEP-COJ)-.5)652,6451,6451 38464 iIIFICCJEP-DOJ)649,6452,6452 3856452 DCJIIDOJEP 386TSIPJIIIPINJ-DOJ/2.)/ISJ-WELCJ+.4-PINJ) 387

    GC TO 652 388649 CCNTINUE 389C SET SCH 40 PIPE THICKNESS. PIPE C P CISH R DIUS ND KNUCKLE R DIUS 390652 IFIOOJ-IO.75)6520,6524,657 3916520 IFICCJ-6.625l6521,6522,6523 3926521 TSEPJIIiTHIKII) 393R A C ~ J I I ~ . 4 2 394RACKJII.84 395GC TO 653 3966522 TSEPJIIITHLKI2J 397KADHJII5.31 398RACKJIII.OI 399GO TC 653 4006523 T ~ E P J 1 I 1 T H I K I 3 l 401RACHJI/6.98 402RACKJIII.33 403GO TO 653 4046524 T S E P J I I i T H I K I ~ l 405RACHJII8.77 406RACKJIII.67 407653 IFITSEPJ-TSEPJIJ656,656,654 408654 WRITE OUTPUT T PE 9,655,TSEPJ 409

    6 5 5 0 F O R ~ A T I IH .5X89HSCHECULE 40 PIPE TOO THIN FOR J CKET SHELL UNDER E 410IXTERN L PRESSURE. REQUIRED THICKNESS IS F7.4, IX 7HINCHES.J 4116550 GO TO 734 412656 TSEPJIITSEPJJ 413C HE C THICKNESS DUE TO I ~ T E R N A L PRESSLRE 414C SET UP CISH R DIUS ND KNUCKLE R DIUS 415657 IFICCJ-10.75)672,672,65E 416658 IFICOJ-4R.J659,667,668 417659IFIDOJ-12.)672,663,660 418660 I F I CO 24. 664,66.3,66 I 4 I 9

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    APPENDIX D (conti,nued)

    661 IF(COJ-30.1665,66.3.662 42066 2 1F ( CO J- 36. '66 :l , 66.3. 66 5 42 1663 KACHJHDCJ 422GC TO 672 423664 IF(CCJ-16.1665,666.665 424665 RADHJNDOJ-2. 425GO Te 6 2 1126666 RACI-JHDCJ-I. 427GO TO 672 428667 RADI J HCC J- 6. 429GC TO 672 430668 IF{COJ-84.)669,663,663 431669 IF(TSEPJ-TSIPJ)670.671,671 432670 I F T S I P J - . 5 j 6 6 ~ f 6 6 3 . 6 6 7 433671 I F I T S E P J - . 5 1 6 6 ~ , 6 6 3 , 6 6 7 434672 RK2JN.C6*OOJ 4 3 ~6720 IF(CCJ-II.1679,679,673 436

    673 IF(TSEPJ-TSIPJ)674,67S,675 437674 RK3JH3.*TSIPJ 438GO TO 676 439675 RK3JN3.*TSEPJ 440676 IF{RK2J-RK3JI678,677,677 441677 RADKJNRK2J 442GO TO 679 443678 RACKJHRK3J 444679CTHIPJNPINJ*RADHJ*{.25*13.+SQRTFIRADHJ/RAOKJ})J/{2.*SJ*WELDJ-.2*PIN 445IJJ 446C TI ICKNESS OF HEAD CUE Te EXTERNAL PRESSLRE 447681 DO 686 1#1,96 448HINI 449RIN8J*.OI5625 450682 TI-EPJNfll 451683 SEGhJN.12*TI-EPJ/RADHJ 452684 SEPI-J#2.*PEXJ*RADI J/IEJ*THEPJ) 453

    6A5 IFISEGHJ-SEPHJJ686.687,687 454686 CCNTINUE 455C ChOOSE CONTROLLING ShELL AND HEAD THICKNESS 456687 IFICOJ-IO.7S)68B,688.697 45768H IF(TSEPJ-TSIPJ)689,689,691 458689 wRITE OUTPUT TAPE 9,69C,TSIPJ 4596 9 0 c r O R ~ A T I IH ,5X89HSCHECULE 40 PIPE TOO THIN FOR JACKET SHELL UNDER 460INTERNAL PRESSLRE. REQUIRED THICKNESS IS F7.4, IX 7HINCHES.) 461

    G TO 734 462691 WRITE OUTPUT TAPE 9,692 4636 9 2 0 F O R ~ A T I IH ,5X8CHSCHEDULE 40 PIPE THICK ENOUGH FOR INTERNAL AND EXT 464IERNAL PRESSLRE ON JACKET SHELL IJ 465693 IF(TSEPJ-THEPJJ694.6930,693C 4666930 1FIT S EPJ - rH PJ J 693 I 696 , 696 4676931 WRITE OUTPUT TAPE 9,6932,THIPJ 468

    6 9 3 2 0 F C R ~ A T I H ,5X92HSCHECULE 40 PIPE CAP TOC THIN FCR JACKET HEAC UNDt 469IR INTEKNAL PRESSURE. RECUIREC T ~ I C K N E S S IS F7.4, IX 7HINCHES./l 470GO TO B 4 471694 WRITE CUTPUT TAPE 9,695,THEPJ 472

    6 9 5 C F C R ~ A T I H .5X92HSCHECULE 40 PIPE CAP TOO THIN FCR JACKET HEAC UNDE 473IR EXTERNAL PRESSURE. REQUIRED THICKNESS IS F7.4. IX 7HINCHES.I) 4746950 GO TO 734 475696 ~ R I T E OUTPUT TAPE 9,696C 4766960 F C R ~ A T I H ,5x79HSCHECULE 40 PIPE THICK ENOUGH FOR INTERNAL AND EXT 477IERNAL PRESSURE ON JACKET HEAD I I 786961 TI- EPJIHSEPJ 479

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    -33-

    APPENDIX D (

    C

    TSJ/lTSEPJTf-,JIHSE PJ6964 IF((COJ-2.-TSJ-CC1-(2.-SPACEIJ7C30.720.720697 IF(TSEPJ-TSIPJI699,698,t9869t1 TSJIITSFPJ

    GO TO 7[0699 TSJIHS I PJ700 DC 702 Ili5,14I F ( TSJ- TH K I I ) 70 1 1 [ I , 102701 TSJNThlKIl JGC TO l i B1[2 CONTINUE103 IFI(OOJ-2.-TSJ-OOI-12.*SPACElllC30,lC4,104

    1030 LINL2+1GC TO 6 ~ 1lC4 I F I T S E P J - T S I P J I 1 0 ~ , l C ~ , 7 0 1105 WRITE CUTPUT TAPE 9.106

    l o 6 0 F C R ~ A T ( J H ,5X54HJACKET SHELL THICKNESS C O N T ~ O L L E O Y INTERNAL PRESISURE JGO TO 7 .9101 WRITE OUTPUT TAPE 9,108

    l o 8 [ F O R ~ A T ( IH ,5X54HJACKET SHELL THICKNESS CONTROLLED Y EXTERNAL PRESISURE I1 C9 IF ( THE P THIP J J 7 I 1 , 7 Ie 7 1 0

    710 TI-'.JIITI-'EPJGC TC 712111 THJIHHIPJ

    712 DC 714 I I i ~ 1 4IF(THJ-THIK(L))713,713,714713 THJIITHIK(I)IF(THJ-TSJJ714,715,715714 CGNT1NUE715 I F ( T H E P . ~ T H I P J J 7 1 8 , 7 1 8 , 7 1 6116 WRITE OUTPUT TAPE 9,717

    7 1 7 0 F O R ~ A T ( IH ,5X53HJACKET hEAD THICKNESS CCNTROLLED PY EXTERNAL PRESSlUREGC TO 72071B WRITE OUTPUT TAPE 9,719

    7 1 9 0 F C R ~ A T ( IH ,5X53HJACKET hEAD THICKNESS CCNTROLLED Y INTERNAL PRESSlURE

    E'NC THICKNESS720 TEIEPJII2.*TSJIFITEIEPJ-.2S1721,72I,722721 IE I EPJ#.25GO TO 124722 IF(TEIEPJ-I .1724,724,72723 TEIEPJItI.724 DIJltDOJ-2.*TSJC7240725WFIGhTS AND COSTSWJSIICENSJ*(SSLJ-I.51*3.14159*CDCJ*OCJ-OIJ*OIJ)/14.*1728.)WJEIICFN\J*TEIEPJ*3.14159*(CIJ-OIJ-DC-DO)/(4.*1728.}IF(THJ-I .)726,727,727726 wJHIICENSJ*ThJ*IDOJ+CCJ/24.+3.+2.-RACKJ/ .)**2-3.14159114.*1728.)7260 GC TC 128727CWJHIICENSJ*THJ*(CCJ+DCJ/24.t3.+2.*RACKJI3.+ThJ)*-2*3.14159/11728.*4I 728 T ~ J W J S + w J E + ~ J I - '

    729 TWJV lTWV+TWJ730 CCSTMJNTWJ*CMPPJ731 Tcas TI'll. TWJV*CFPP

    4804814824834844854861181488IIB9490491492493119449549649749849950050150250350115055116507508509510511512513511151551/))175185195205215225235211

    5 2 ~526527528529530)31532533534)355365 3153853?

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    -34-

    l\I?ENUIX D (cont inued)

    732 T C C S T ~ . C O S T ~ + C C S T M J 540733 T C O S T I f C O S T B + T C O S T ~ 541734CWRITE CUTPUT TAPE 9,735,A5J,A6J,A7J,TEMPJ.SSLRJ,OCJ,TSJ,CIJ.CO. 542I T E l E P J , T H J , R A D H J , R A C K J . S F , D E ~ S J . O E N S Q J . P I N J , P E X J . E J 543

    7 3 5 [ F O R ~ A T { I H ,4X24HMATERIAL OF CONSTRUCTION 7X3A61 5x 3HOESIGN TEMP 544IF F37.01 5X 34HSTRAIGHT SLOE/VESSEL STRAIGHT SIDE F19.31 5X 20HOUT 5452SlCE DIAMETER IN. F34 41 5X 19H5HELL THICKNESS IN. F35 41 5x 20HEN 54630 Cl;TSICE DIAM IN. F ~ 4 . 4 1 5X 19HEND INSIDE CLAM l " . F35 41 5X 17HE 5474NC THICKNESS IN. F37 41 5X IBHHEAO THICKNESS IN. F36 41 5X 2DHHEAD 5485 DISH RACIUS IN. F33 31 5X 23HHEAD K ~ U C K L E RACIUS F30.31 5X24H 5496HEAC STRAIGHT FLANGE LN. F28 21 5X 23HMETAL DENSITY LAS/CU FT F30. 5507 ~ 1 5X 24HMETAL CENSLTY LAS/CU IN. F3C 411 SX 2BHDESIGN INTERNAL PR 551BESSl;RE PSI F23.11 5X 28HDESIGN E X T E R ~ A L PRESSURE PSI F23.11 5X 25H 5529MCDULUS OF ELASTICITY PSI 23XEI 1.5) 553736CWRITE OUTPUT TAPE 9 , 7 3 7 , S J , W E L C J , W J S , W J E , W J H , T W J , T W J V . C ~ P P J , C O S T M J 554

    I , T C O S T ~ . T C C S T B , T C O S T I 555737CFORI"AT IH ,4X 32HMAX ALLOWABLE TENSILE STRESS PSI FIB.OI 5X 26HWFL 55610 EFFICIENCY DEC.FRACT. F27 311 5X 19HwEIGHT OF SHELL LBS F34.31 5 5572X 21HWEIGHT OF ONE END LBS F32 31 5X IBHWEIGHT CF HEAO LBS F35 31 55835X 26HTGTAL WELGHT OF JACKET LqS F27 31 5X 33HTOTAL WEIGHT OF JACK 5594ET+VESSEL LBS F20 311 5X 22HJACKET METAL COST $/LA F31.31 5X 2DHJA 5605CKET METAL COST $ F33 31 5X 27HJACKET+VESSEL ~ E T A L COST $ F26.31 56165X 25HTOTAL FA8RICATION COST $ F28 31 3JHTOTAL l;NIT COST(JACKE 5627T+VESStL) $ F20.3 II 563738 WRITE OUTPUT TAPE 9,739 5647390FCRI"ATlIH ,4X92H(JACKET E lD A S S U ~ E O T 8E TWICE THE SHELL THICKNES 565IS eUT LIMITED TO BETWEEN 0.25 AND 1 [ IN.)) 5667390IFIJHEC)7391.7391,7393 5677391 WRITE OUTPUT TAPE 9.7392 5687392 FORI-'AT(IH .4X 40HIJACKET ON STRAIGHT SrCE OF VESSEL ONLY)) 569O TC 740 l7f)7393 WRITE OUTPUT TAPE 9,7394 5717394 F C R ~ A T ( I H .qX 4CH(JACKET HAS ONE AS,..E TORISPHERICAL HEAO)) 572740 IF(JLOC)597,597,741 573741 WRITE CUTPUT TAPE 9,52IC,HSEPCJ,wTSRJ ')74750 GC TO 597 575ENe 576

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    APPENDIX F

    Deck setup for Central Data Processing Facility, ORGDP*rD*Charge*TAPE 9, OUTPUT) 10, INPUT )*DUMP * 1000, 77460, D*EXECUTE*TYPE BINARY)

    Binary Deck of Cards)*DATAList of inside diameters f i rst card)List of outside diameters second card)List of thicknesses third card)Data cards for vessel design)

    Note: Fortran deck may be used by changing TYPE card toFORTRAN and using Fortran deck

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    APPENDIX G UNFIRED PRESSURE VESSEl DESI GN DATA SHEET

    WRITTEN /e ;vj I/ o XVessel Design Data:

    Capacity,cu It

    Jacket Design Data:

    Jacket StraightSide/VesselStraight Side

    NOTES:

    FreeBoordRatio

    Min. SpaceBetweenVe ... I and

    Jacket ID

    H\7

    StraightSide/Ratio

    DesignExternalPressure,osi

    HeodStraightFlange,in.

    DesignInternalres ure lpsi

    ModulusofElosticity,psi

    DesignTemp.,OF

    39

    t.AaximumAllowableTensile Stresspsi

    ModulusofEiasticitYIpsi

    49

    DesignTemp.,of

    MaximumAllowableTensite, Stresspsi

    D .. gnExternalPressure,psi

    MetalCost,lIb

    DesignInternolPressure,

    psi

    WeldEff.,Dec.

    J

    UNCLASSIFIEDORNL-LR-DWG 71757

    3

    4

    1. All decimal paints are coded to the extreme right of the field and do not take up space. However,,, decimal paint may be locoted in any other .pace and will override the printed paint.(See: Heod ... roight flange in card No. 1).2. Use any Fortron characters.3. Only one density value required.4. The final shell and head thicknesses of the vessel are selected from on internal list by selecting the next larger size. To allow 0 smoll overage above one std. thickness before choosing thenext lorger siLe, insert allowable excess 0 decimal fraction of std. thickness.5. All four dota cords must be included for each vessel.6. J: f 0 jacket is to be designed, insert 11\7. H: If a iacket is to have a head, insert 1 . Jacket may have no more than one head

    I\..AJ0'\I

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    -37-

    APPENDIX G continued)

    S ~ E ~ L THICKNESS CONTROLLED BY EXTERNAL PRESSUREHEAD THICKNESS C O ~ T R O L L E O By EX1ERNAL PRESSUREVESSEL NUMBERMATERIAL O CONSTRUCTiONDESIGN TEt'' ? FDESIGN CAPACITY CU FTFREEBOARD RATIOVESSEL VOLUME CUONE HEAD DISH VOLUME GALSTRAIGHT LENGTH IOUTSIDE OIAMOUTSIDE DIAMETER IN.SHELL T H I C K N F S ~ TN.SMELL LENGTH I ~ .

    H ~ A D T ~ I C ~ ~ E S S IN.MEAD DISH ~ A O I U SHEAD KNUCKLE R ~ D I U 5 IN,HEAD STRAIGHT FLANGE IN,

    w ~ l G H T OF S H E L ~ LBS~ E I G r l T OF ONE HEAD L STOTAL WEIGHT OF v E S S E ~ LSSMETAL DENSITY LB PER CU FTMETAL D E ~ S I T Y PER IN.DESIGN ExTERNAL PRESSURE PSIDESIGN INTERNAL PRESSURE PSIMODULUS OF ELASTICITY PSIMAX ALLOWABLE TENSILE STRESS PSICORROSION ALLOWANCE IN.

    EXAMPl ESA-240 3Q4L SS312.60.0001.4385.949

    2 5 ~ 0 62.50042.0[)000. 0 250102.0000.625040.0002 520I .502402.491333.8053070.100

    501.0000,95.020.0U.26700E 0812 :S48.

    ALLOWANCE OVER STO THIK. DEC.FRACT.wELD EFFICIENCY D E C . f R ~ C TO. 12500.040U0.800

    METAL COST 3; PERFABRICATION COSTMETAL COSl TOTALFABRICATION COSTTOTAL UN IT COST

    LB$ pER

    j

    TOTAL.:h

    LB

    f;

    0.65002,50001995,5657675.2509070.815

    THE ABOVE C ~ L C U L A T I O N IS FOR ASME TORlSPHERICAL HEAD)

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    -38-

    APPENDIX G (continued)

    JACKET FOR vESSEL NUMBER EXAMPLEJACKET SHELL THICKNESS c O N T R O L ~ E U BY EXTERNAL PRESSUREJACKET HEAn THICKNESS CONTROLLED By INTERNAL PRESSURE

    MATERIAL OF CONSTRUCTiON SA-24Q,DESIGN H:MP FSTRAIGHT SloE/VESSEL STRAIGHT S OEOUTSIDE D I A ~ E T E RSHELL THICKNESS TN.END OUTSIDE OIAM IN.END INSIDE DIAM IN.END T H I C K N ~ S S INHE D THICKNESS IN.HEAD DISH RADIUS IN,HE D KNUCKLE RADIUS IN.HEAD STRAIGHT FLANGE IN.METAL DENSITY LHS/CU fTMETAL DENSITY LSS/Cu IN.DESIGN INTERNAL PRESSURE PSIDESIGN EXTERNAL PRESSURE PSIMODULUS OF ELASTIClTY PSIM X ALLOWABLE TENSILE STRESS PSiW E ~ D EFFICIENCY DEC.FRACT.WEIGHT OF SHELL LBSwEtGHT OF ONE END L8SWEIGHT OF HEAD LBSTOTAL WEIGHT OF JACKET LSSTOTAL WEIGHT OF JACKET.VtSSEL lESJACKET METAL COST /LBJACKET METAL CuST $JACKET+vESSEL METAL CUST $TOTAL ~ A k l C A T l O N COSTTOTAL IJNIT COST(JACKEr+VESSEL) 6

    304L SS312.0.75048.00000.250047.500042.0000O.SQOO0.375042.0002.8801 ,50501.00U-D.

    Bu.O15.0U.267DlJE US12c;48.0.800839.954

    56 045257,5581153.557422 ;.6570,650749,8122745,37710559.14313 304,52T

    (JACKET END ASSUMED TO 8E TWICe THE SHELL THICKNESS BUT LIMITEDTO BEtWEEN 0,25 ND 1.0 IN.) J ~ C K E T HAS ONE SME TORISPHER1CAL HEAD)

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    -39-

    DISTRIBUTION

    l C. E. Bettis 38. J. P. Nichols2. E. s. 39 E. L. Nicholson3 G. B. Berry 40. F. L Peishel4. R. E. Blanco 4I. T. W Pickel5 J. 0 Blomeke 42. C. E. Prince6. B. F. Bottenfield 43. P. L. Robertson7 E. J. Breeding 44. A. M. Rom8. J. C. Bresee 45 J. B. Ruch9 R. B. 46. O. w. Russ K-I00710. R. E. Brooksbank 47. A. D. Hyon

    l I F. N. Browder 48. W. F. Schaffer12. K B. Brown 49 R. W. Schneider13 W. D. Burch 50. E. M. Shank14. W. H. Carr Jr. 5I. T. Shapiro15 W. L. Carter 52. L. B. Shappert16. G. Cathers 53 M. J. Skinner17 J. M. Chandler 54. S. H. Smiley18. G. A, Cristy 55 F. Sneider19 F. L. Culler 56. W. G. Stockdale20. D. E. Ferguson 57 J. C. Suddath21- E. J. Frederick 58. W. E. Unger22. H. E. Goeller 59 c. D. Watson23 H. B. Graham 60. H. o. Watson24. C. E. Guthrie 6I. M. E. Whatley25 P. A. Haas 62. W. K. Whitson Jr.26. F. L. Hannon 63. W. R. WhitsonF. E. Harrington 64. W. R. WinsbroW. E. Heckert Y-12 65. O. O. Yarbro29 J M. Holmes 66-67. Central Research30. R. W Horton Library31- B. B Klima 68. Document Reference32. E. Lamb Section33 J. W. Landry 69 Laboratory Records34. R. B. Lindauer 73 Laboratory Records RC)35 J. T. Long 74-89 DTIE36. H. G. MacPherson 90. Research and Development37 R. P. Milford Division ORO)

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