eksempel - momentbelastet søjle

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  • 8/9/2019 Eksempel - Momentbelastet søjle

    1/3

    Aarhus UniversitySchool of Engineering

    Department of Mechanical Engineering   59

    Example – axial loaded member with bending moment.

    The steel column shown below is free at the upper end and supported by a fixed support at the lower

    end. The column is free to deflect in both y- and z-direction.

    The design load at the column is:

    Axial force NEd = 100 kN

    Transverse force: FEd = 20 kN (in z-direction)

    The cross section is a rolled I- section type IPE400, see cross-section below. Steel material is S235,

    normal control class. IPE400 is a class 3 cross-section.

    t =13.5f

    t

    =8.6

    y

    zx

            b    =        1        8        0

    h=400

        w    =        3        9        0        0

    FEd

    Section A-A

    M =Ed F  l Ed

                l

    NEd

    y,

    A A

    Bending moment diagram

     Question:

    Check the resistance of the column for the attached load.

    Solution:

    Cross-section values for IPE400:

    mmi

    mmW mm I 

    mmi

    mmW mm I 

    mm A

     z

     z z

     y

     y y

    5.39

    10146 and 102.13

    165

    101160 and 103.231

    1045.8

    :table-IPE400From

    3326

    3346

    23

    =

    ⋅=⋅=

    =

    ⋅=⋅=

    ⋅=

     

    43

    69

    10514

    10490

    mm I 

    mm I 

    v

    w

    ⋅=

    ⋅= 

    The column length:

    mml Lcr  7800390022   =⋅=⋅=   (concerning both the y-axis and the z-axis).

  • 8/9/2019 Eksempel - Momentbelastet søjle

    2/3

    Aarhus UniversitySchool of Engineering

    Department of Mechanical Engineering   60

    For IPE400: 2.2180

    400==

    b

    Slenderness:

    6.1)and6.2Tablesee(0.21a""curvebuckling50.019.93

    165

    7800

    9.93.=⇒→=

    ⋅=

    ⋅=⋅=  y

     y

    cr 

     ycr 

     y

     yi

     L

     N  f  A α 

    ε λ   

    6.1)and6.2Tablesee(0.34b""curvebuckling10.219.93

    5.39

    7800

    9.93.=⇒→=

    ⋅=

    ⋅=

    ⋅=  z

     z

    cr 

     zcr 

     y

     z

    i

     L

     N 

     f  Aα 

    ε λ   

    Buckling reduction factor:

    ( )[ ]   ( )[ ] 66.050.02.050.021.015.02.015.0

    6.4)Figurefrom(or92.050.066.066.0

    11

    22

    2222

    =+−⋅+=+−+=

    =

    −+

    =

    −+

    =

     y y y y

     y y y

     y

    λ λ α φ 

    λ φ φ 

     χ 

     

    ( )[ ]   ( )[ ] 03.310.22.010.234.015.02.015.0

    6.4)Figurefrom(or19.010.203.303.3

    11

    22

    2222

    =+−⋅+=+−+=

    =

    −+

    =

    −+

    =

     z z z z

     z z z

     z

    λ λ α φ 

    λ φ φ  χ 

     

    Design resistance for the axial force:

    07.0104.1522

    10100

    104.152220.1

    2351045.892.0

    3

    3

    ,,

    33

    1

    ,,

    =⋅

    ⋅==

    ⋅=⋅⋅⋅

    =⋅⋅

    =

     y Rd b

     Ed 

     y

     M 

     y y

     y Rd b

     N  N n

     N  f  A

     N γ  

     χ 

     

    32.0104.314

    10100

    104.31420.1

    2351045.819.0

    3

    3

    ,,

    33

    1

    ,,

    =⋅

    ⋅==

    ⋅=⋅⋅⋅

    =⋅⋅

    =

     z Rd b

     Ed 

     z

     M 

     y z

     z Rd b

     N 

     N n

     N  f  A

     N γ  

     χ 

     

    Interaction factors (see Table B1, B2 and B3):

    ( )   ( ) 92.06.0192.007.050.06.0190.0)0 and 0 :B3(Table90.0

    6.016.01

    h

    =⇒⋅+≤=⋅⋅+⋅=

    ===

    ⋅+≤⋅⋅+=

     yy ymy yy

    hmy

     ymy y ymy yy

    k nC k 

     M C 

    nC nC k 

    α 

    λ 

     

    0

    789.320

    98.098.032.025.090.0

    05.0194.032.0

    25.090.0

    10.205.01

    )0 and 0 :B1(Table90.0

    25.0

    05.01

    25.0

    05.01

    ,

    ,

    h

    =

    =⋅=⋅=

    ⋅⋅=

    =⇒=⋅−

    −≥=⋅−

    ⋅−=

    ===

    ⋅−

    −≥⋅−

    ⋅−=

     z

     Ed  Ed  y

     yd  y LT 

     Ed  y

     y

     zy zy

    hmLT 

     z

    mLT 

     z

    mLT 

     z zy

    m

    kNmlF  M 

     f W 

     M m

    k k 

     M C 

    nC 

    nC 

     χ 

    α 

    λ 

     

  • 8/9/2019 Eksempel - Momentbelastet søjle

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    Aarhus UniversitySchool of Engineering

    Department of Mechanical Engineering   61

    The lateral-torsional buckling reduction factor χ LT must be found (same procedure as in Example 2 on

    page 55):

    48.2104906.2

    390010514 

    9

    232

    =⋅⋅⋅

    ⋅⋅⋅=

    ⋅⋅=⋅

     E 

     E 

     I  E 

    l I Glk 

    w

    v  

     Nmmhl

     I  E lk  M  t 

     z E 

    6

    2

    622

    2

    22

    109.4425.3863900

    102.1321000048.21

    21

    2⋅=⋅

    ⋅⋅⋅

     

      

     +⋅=⋅

    ⋅⋅

     

      

        ⋅+⋅=

    π 

    π 

    π 

    π  

    ( ) ( )

     Nmm M c M 

    c

    cc

    lk 

    cccc

     E  LT cr 

     LT 

     LT 

    66

    2

    21

    2

    2

    2

    2

    2

    2

    21

    103.354109.44280.0

    80.049.24

    28.1

    49.24

    28.1130.1

    52pageseeflange,upperat theload- 1-

    6.6Tablesee- 28.16.6;Tablesee-30.1

    49.248.24

     4

     44

    1

    ⋅=⋅⋅=⋅=

    =

     

     

     

     

    +

    −+

    +⋅=

    =

    ==

    =⋅=⋅⋅=

     

     

     

     

    +

    ⋅++

    +⋅=

     β 

    π π κ 

    κ  β 

    κ 

     

    88.0 103.354

    235101160 

    6

    3

    =⋅

    ⋅⋅=

    ⋅=

    cr 

     y y

     LT  M 

     f W λ   

    ( )[ ]   ( )[ ]

    51.023510116068.0

    20.11078

    )71.088.075.091.091.0

    1 :case(alternat. 68.0

    88.00.10.1

    6.3Tablesee- 34.06.4)(Tablebcurvebucklingonimperfecti22.25.13

    400

    0.188.02.088.034.015.02.015.0

    1

    3

    6,

    2222

    22

    22

    =⋅⋅⋅

    ⋅⋅=

    ⋅⋅=

    =

    ⋅−+

    ==

    −+

    =

    =⇒⇒>==

    =+−+=+−+=

    −+

    =

     yd  y LT 

     Ed  y

     y

     LT  LT 

     LT 

     LT  LT  LT  LT 

     LT  LT  LT 

     LT 

     f W 

     M m

    b

    h

     χ 

     χ  χ 

    α 

    λ λ α φ 

    λ φ φ  χ 

     

    Criteria, which must be satisfied:

    O.K. 154.051.092.007.01