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12/14/11 1 Topic 8 Columns Design Prof Dr Shahrin Mohammad Structural Steel and Timber Design SAB3233 Structural Steel Design Topic 1 Overview Topic 4 – Design of steel structures (BS EN 1993) Topic 3 –AcKons on Structures (BS EN 1991) Topic 5 – CrosssecKon classificaKon Topic 2 Basis of Structural Design (BS EN 1990) Topic 6 – Laterally restrained beams Topic 7 – Laterally unrestrained beams Topic 8 – Columns Design Topic 9 – Trusses Topic 10 ConnecKons

Topic 8 - steel columns

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Page 1: Topic 8 - steel columns

12/14/11

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Topic  8    Columns  Design  

       

Prof  Dr  Shahrin  Mohammad  

Structural  Steel  and  Timber  Design  SAB3233  

Structural  Steel  Design  

Topic  1  -­‐  Overview  

Topic  4  –  Design  of  steel  structures  (BS  EN  1993)  

 Topic  3  –AcKons  on  

Structures      (BS  EN  1991)  

 Topic  5  –  Cross-­‐secKon  

classificaKon  

Topic  2  -­‐  Basis  of  Structural  Design  (BS  EN  1990)  

Topic  6  –  Laterally  restrained  beams  

Topic  7  –  Laterally  unrestrained  beams  

Topic  8  –  Columns  Design  

Topic  9  –  Trusses  

Topic  10  -­‐  ConnecKons  

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   Columns  subjected  to  axial  load  

       

Prof  Dr  Shahrin  Mohammad  

Structural  Steel  and  Timber  Design  SAB3233  

Mx,t My,t

x

y

Mx,b

My,b Squashing, normally occurs in short column

Overall flexural buckling

Torsional buckling

Local buckling

NEd   NEd   NEd   NEd   NEd  

NEd  =  Design  value  of  compression  force      

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5  

! compression  members  subject  to    §  axial  compression  only    §  no  bending  

! however  in  pracKcally  real  columns  are  subject  to  §  eccentriciKes  of  axial  loads    §  transverse  forces  

! the  treatment  disKnguishes  between  §  stocky  columns,  and  §  slender  columns  

6  

Stocky  columns    The  characterisKcs  of  stocky  columns  are  

•   very  low  slenderness  •   unaffected  by  overall  buckling  

   The  compressive  strength  of  stocky  columns  is      

•   dictated  by  the  cross-­‐secKon  •   a  funcKon  of  the  secKon  classificaKon    

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Slender  Steel  Columns  

   Slender  columns  present  a  quasi  elasKc  buckling  behaviour  

   Euler  criKcal  stress    λ  =  Lcr  /  r,  where      r      is  radius  of  gyraKon  

           Lcr  is  the  buckling  length  

2

2

λπ

σE

cr =

Failure  by  yielding  

Failure  by  buckling  

Euler  buckling  curve  

λ

σ

fy

λ1

Euler  buckling  curve  and  modes  

of  failure  

8  

Behaviour  of  real    steel  columns    

q  columns  of  medium  slenderness  are  very  sensiKve  to  the  effects  of  imperfecKons  

q  inelasKc  buckling  occurs  before  the  Euler  buckling  load  due  to  various  imperfecKons    §  iniKal  out-­‐of-­‐straightness  §  residual  stresses  §  eccentricity  of  axial  applied  loads  §  strain-­‐hardening  

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Effects  of  imperfecKons  

•  structural  imperfecKons  most  important  for  intermediated  columns  

•  this  represents  most  pracKcal  columns    

•  lower  bound  curve  is  obtained  from  a  staKsKcal  analysis  of  test  results  

10  

Effect  of  imperfecKons  in  relaKon  to  slenderness  

­  Slender  column  ⚈  largely  unaffected  by  imperfecKons  ⚈  ulKmate  failure  load  ≈  Euler  load  (Ncr)    ⚈  independent  of  the  yield  stress  

­  Intermmediate  column  ⚈  imperfecKons  important  ⚈  failure  load  less  than  Euler  load    ⚈  out-­‐of-­‐straightness  and  residual  stresses  are  the  most  significant  imperfecKons  

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Residual  stresses  pa_erns  

Typical  residual  stress  pa_ern  

y

y

y

0 , 3 f

0 , 2 f

0 , 2 f

∼ compression

tension

compression

+ =

σ R N / A σ n f y < σ n f y

f y

o r =

reaching

CombinaKon  with  axial  stresses  

•  combined  with  axial  stresses  cause  yielding  •  effecKve  area  reduced  

Modify  

IniKal  out-­‐of-­‐straightness  

!  induces  bending  moments    

Yielded zones

Combined  effect  of  imperfec0ons  and  axial  load    

! bending  stress  σB  ! residual  stress,  σR  ! applied  axial  stress,  NEd/A  

+ +

P / A σ R

=

σ B σ max

NEd  

NEd  

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Buckling  resistance  in  axial  compression  

The  design  buckling  resistance  of  a  compression  member      

Nb.Rd = χAfyγM1

1.

M

yeff

Rdb

fAN

γχ=

for  Class  1,  2  and  3  cross  secKon  

for  Class  4  cross  secKon  

where  χ  a  reducKon  factor  and  is  related  to  the  reference  slenderness    Buckling  curves  plo_ed  as  χ  versus  reference  slenderness  raKo  

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European  buckling  curves    (Cl  6.3.1.2)  

Ncr is the elastic critical force for the relevant buckling mode based on the gross cross sectional properties.

16  

European  buckling  curves  

Based  on  experiment  more  than  1000  tests  secKon  Range  of  slenderness  raKos  between  55  and  160  

•  Based  on  a  half  sine-­‐wave  geometric  imperfecKon  =  L/1000    

•  residual  stresses  related  to  secKon  type  

•  4  curves  apply  to  different  cross-­‐secKon  types  corresponding  to  different  values  of  the  imperfecKon  factor  α

Modify  

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ImperfecKon  factor  a  

•   α  depends  on    §  the  shape  of  the  column  cross-­‐secKon    §  the  direcKon  of  buckling  (y  or  z  axis)    §  the  fabricaKon  process  (hot-­‐rolled,  welded  or  cold-­‐formed  

•  imperfecKon  factors  given  in  Table  6.1      

Non  dimensional  slenderness,  ___λ

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SelecKon  of  appropriate  buckling  curve  

Table 6.2 helps with the selection of the appropriate buckling curve

Modify  

Example  1  :  Design  of  an  axially  loaded  column  

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   Columns  subjected  to  combined  

bending  and  axial  load            

Prof  Dr  Shahrin  Mohammad  

Structural  Steel  and  Timber  Design  SAB3233  

Mz,t  

y    

z  

My,t  Mz,t  

My,b  

Mz,b  

y    

z  

My,t  Mz,t  

My,b  

Mz,b  

y    

z  Pin  

connecKon  Pin  

connecKon  Pin  

connecKon  

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Mz,t  

y    

z  

My,t  Mz,t  

My,b  

Mz,b  

y    

z  

My,t  Mz,t  

My,b  

y    

z  Mz,b  

My,b  

Mz,b  

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simple  construcKon  

‘Simple  construcKon’  is  commonly  used  for  the  design  of  mulK-­‐storey  buildings  

•  Beams  are  designed  as  simply  supported  

•  Columns  are  designed  for  nominal  moments  arising  from  the  eccentricity  at  the  beam-­‐to-­‐column  connecKon.  

NEd

Nb,z,Rd

+My,Ed

Mb,Rd

+1.5 Mz,Ed

Mc,z,Rd

≤1

The  moment  components  are  small  for  simple  construcKon,  the  interacKon  factors  can  be  conservaKvely  simplified  to  :  

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Example  1  :  Design  of  column  with  combined  bending  and  axial  load  

Thank You