Aisc Asd-89 Example 002

Embed Size (px)

Citation preview

  • 8/11/2019 Aisc Asd-89 Example 002

    1/5

    Software VerificationPROGRAM NAME: ETABS 2013

    REVISION NO.: 0

    AISC ASD-89 Example 002 - 1

    AISC ASD-89 Example 002

    WIDE FLANGE MEMBER UNDER COMPRESSION

    EXAMPLE DESCRIPTION

    The column design features for the AISC ASD-89 code are checked for the frame

    shown below. This frame is presented in the Allowable Stress Design Manual ofSteel Construction, Ninth Edition, 1989, Example 3, Pages 3-6 and 3-7. The

    columnKfactors were overwritten to a value of 2.13 to match the example. The

    transverse direction was assumed to be continuously supported. Two point loadsof 560 kips are applied at the tops of each column. The ratio of allow axial stress,Fa, to the actual,fa, was checked and compared to the referenced design code.

    GEOMETRY,PROPERTIES AND LOADING

    TECHNICAL FEATURES TESTED

    Section compactness check (compression) Member compression capacity

  • 8/11/2019 Aisc Asd-89 Example 002

    2/5

    Software VerificationPROGRAM NAME: ETABS 2013

    REVISION NO.: 0

    AISC ASD-89 Example 002 - 2

    RESULTS COMPARISON

    Independent results are taken fromAllowable Stress Design Manual of Steel

    Construction, Ninth Edition, 1989, Example 3, Pages 3-6 and 3-7.

    Output Parameter ETABS IndependentPercent

    Difference

    Compactness Compact Compact 0.00%

    Design Axial Stress,fa(ksi) 15.86 15.86 0.00%

    Allowable Axial Stress,

    Fa(ksi)

    16.47 16.47 0.00%

    COMPUTER FILE: AISCASD-89EX002

    CONCLUSION

    The results show an exact comparison with the independent results.

  • 8/11/2019 Aisc Asd-89 Example 002

    3/5

    Software VerificationPROGRAM NAME: ETABS 2013

    REVISION NO.: 0

    AISC ASD-89 Example 002 - 3

    HAND CALCULATION

    Properties:

    Material: A36 Steel

    E = 29,000 ksi,Fy = 36 ksi

    Section: W12x120:

    bf= 12.32in, tf= 1.105in, d =13.12 in, tw=0.71 in

    A = 35.3 in2

    rx=5.5056 in

    Member:

    K= 2.13

    L= 15 ft

    Loadings:

    P = 560 kips

    Design Axial Stress:

    560

    35.3a

    Pf

    A

    15.86 ksia

    f

    Compactness:

    Localized Buckling for Flange:

    1 2 . 3 25 . 5 7 5

    2 2 1 .1 0 5

    f

    f

    b

    t

    6 5 6 51 0 . 8 3

    3 6p

    yF

    p , No localized flange buckling

    Flange is Compact.

  • 8/11/2019 Aisc Asd-89 Example 002

    4/5

    Software VerificationPROGRAM NAME: ETABS 2013

    REVISION NO.: 0

    AISC ASD-89 Example 002 - 4

    Localized Buckling for Web:

    15.860.44

    36

    a

    y

    f

    F

    13.1218.48

    0.71w

    d

    t

    Since 0 .4 4 0 .1 6a

    y

    f

    F

    2 5 7 2 5 74 2 . 8 3

    3 6p

    yF

    p , No localized web buckling

    Web is Compact.

    Section is Compact.

    Member Compression Capacity

    638.69

    5056.5

    121513.2

    x

    x

    r

    KL

    2 2

    2 2 2 9 0 0 01 2 6 . 0 9 9

    3 6

    c

    y

    EC

    F

    552.0

    099.126

    638.69

    c

    x

    x

    C

    r

    KL

    c

    x

    x

    C

    r

    KL

  • 8/11/2019 Aisc Asd-89 Example 002

    5/5

    Software VerificationPROGRAM NAME: ETABS 2013

    REVISION NO.: 0

    AISC ASD-89 Example 002 - 5

    3

    2

    8

    1

    8

    3

    3

    5

    2

    10.1

    c

    xx

    c

    xx

    y

    c

    xx

    a

    C

    rKL

    C

    rKL

    FC

    rKL

    F

    3

    2

    552.0

    8

    1552.0

    8

    3

    3

    5

    36552.0

    2

    10.1

    a

    F

    16.47 ksia

    F