7-column design shig

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7-Column Design Shig

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  • Column Design(4.11-13)

    MAE 316 Strength of Mechanical ComponentsY. Zhu

    Column Design1

  • Introduction

    Column Design2

    Long columns fail structurally (buckling failure) Short columns fail materially (yielding failure) We will examine buckling failure first, and then transition

    to yielding failure. P

    P

    Long

    2

    2

    LEIPcr

    P

    P

    ShortAP crcr

  • Buckling of Columns (6.2) For a simply supported beam (pin-pin)

    Column Design3

    y, v

    x

    F.B.D y, v

    v(x)

    0

    )(

    )()(

    2

    2

    2

    2

    PvdxvdEI

    PvxMdxvdEI

    xPvxM

    The solution to the above O.D.E is:

    xEIPBx

    EIPAxv cossin)(

  • Buckling of Columns (6.2)

    Apply boundary conditions: v(0)=0 & v(L)=0

    Either A = 0 (trivial solution, no displacement) or

    The critical load is then

    The lowest critical load (called the Euler buckling load) occurs when n=1.

    Column Design4

    xEIPBx

    EIPAxv cossin)(

    0sin&0 LEIPAB

    nLEIPL

    EIP 0sin where n = 1, 2,

    22)(LEInPcr

    2

    2

    LEIPcr

  • Buckling of Columns (6.2) The corresponding deflection at the critical load is

    The beam deflects in a half sine wave.

    The amplitude A of the buckled beam cannotbe determined by this analysis. It is finite, however. Non-linear analysis is required to proceed further.

    Column Design5

    LxAxv sin)(

    Pcr

    A

  • Buckling of Columns (6.2) Define the radius of gyration as

    Pcr can be written as

    If L/rg is large, the beam is long and slender. If L/rg is small, the beam is short and stumpy.

    To account for different boundary conditions (other than pin-pin), use effective length, Le.

    Column Design6

    AIrg 2

    2

    2

    )/( gcr

    rLE

    AP

    crge

    cr

    rLE

    AP 2

    2

    )/(

  • Buckling of Columns (6.2) Effective lengths for various boundary conditions

    Design values (AISI)

    Column Design7

    (a) fixed-free, (b) pin-pin, (c) fixed-pin, (d) fixed-fixed, (e) fixed-non-rotating

    (a) Le = 2.1L, (b) Le = L, (c) Le = 0.8L, (d) Le = 0.65L, (e) Le = 1.2L

  • Critical Stress (6.3) Plot cr=Pcr/A vs. L/rg

    Long column: buckling occurs elastically before the yield stress is reached. Short column: material failure occurs inelastically beyond the yield stress. A Johnson Curve can be used to determine the stress for an intermediate

    column

    Column Design8

    ?

    No failure

    Failure

    Sy

    Johnson Curve

    Note:Sy = yield strength = ySu = ultimate strength = uSp = proportional limit

  • Critical Stress (6.3) Johnson equation

    As Le/rg 0, Pcr/A Sy To find the transition point (Le/rg)c between the Johnson and

    Euler regions

    Column Design9

    2

    2

    2

    4

    g

    eyy

    cr

    rL

    ES

    SAP

    ycg

    e

    g

    eyy

    SE

    rL

    rL

    ES

    S

    rgLe

    E

    JohnsonEuler

    2

    2

    2

    2

    2

    2

    2

    4

  • Design of Columns (6.6) Procedure

    Calculate (Le/rg)c and Le/rg If Le/rg (Le/rg)c use Eulers equation

    If Le/rg (Le/rg)c use Johnsons equation

    Notice we havent included factor of safety yet

    Column Design10

    crge

    cr

    rLE

    AP 2

    2

    )/(

    2

    2

    2

    4

    g

    eyy

    cr

    rL

    ES

    SAP

  • ExampleFind the required outer diameter, with F.S.=3, for the column shownbelow. Assume P = 15 kN, L = 50 mm, t = 5 mm, Sy = 372 MPa, E =207,000 MPa, and the material is 1018 cold-drawn steel.

    Column Design11

    t

    do

  • ExampleFind the maximum allowable force, Fmax, that can be applied withoutcausing pipe to buckle. Assume L = 12 ft, b = 5 ft, do = 2 in, t = 0.5 in,and the material is low carbon steel.

    Column Design12

    t

    do

    F

    L

    b