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Steel Structures
N-W.F.P University of Engineering &
Technology Peshawar
CE - 411
Instructor: Prof. Dr. Shahzad Rahman
Lecturer: Engr. Kamran Ayub
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Example Problem 1
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Example Problem 1(Contd.)
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Example Problem 1(Contd.)
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Example Problem 2 - LRFD
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Example Problem 2 (Contd.)
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Example Problem 2 (Contd.)
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Example Problem 2 (Contd.)
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Example Problem 3
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Example Problem 3 (Contd.)
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Example Problem 3 (Contd.)
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Example Problem 3 (Contd.)
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Example Problem 3 (Contd.)
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KL is called effective length of column and K
effective length factor.
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Effective length factors (AISC manual)
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EFFECTIVE LENGTH OF
COLUMNS IN FRAMES So far, we have looked at the buckling strength of
individual columns. These columns had various
boundary conditions at the ends, but they werenot connected to other members with moment
(fix) connections.
The effective length factor K for the buckling of an
individual column can be obtained for theappropriate end conditions from Table C-C2.1 of
the AISC Manual
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Columns in Frames
However, when these individual columns
are part of a frame, their ends are
connected to other members (beams etc.).
These frames are sometimes braced and
sometimes unbraced.
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A Braced frame is one in which a sideway(joint translation) is prevented by means of
bracing, shear walls, or lateral support fromadjoining structure.
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A UnBraced does not have any bracingand must depend on stiffness of its ownmembers and rotational rigidity of joints
between frame members to prevent lateralbuckling.
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Conclusions
Critical loads for a column depends on
its stiffness relative to that of beamsframing into it and
Presence or absence of restraint to
lateral displacement of its ends.
Effective length coefficient increases with
decreasing stiffness of the beam and
becomes unity with zero stiffness.
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Braced & Unbraced Frames Similarly you can analyze
multibay, multistory frames.
Assumptions Subjected to vertical loads only
All columns become unstable
simultaneously
All joint rotations at floor are equal Restraining moment distributed in
proportion to stiffnesses.
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Method of Analysis First, you have to determine whether the
column is part of a braced frame or an
unbraced (moment resisting) frame. Then, you have to determine the relative
rigidity factor G for both ends of the column
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G is defined as the ratio of the summationof the rigidity (EI/L) of all columns comingtogether at an end to the summation of therigidity (EI/L) of all beams coming together
at the same end.
G =
It must be calculated for both ends of the
column.
b
b
c
c
L
IE
L
IE
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Then, you can determine the effective lengthfactor K for the column using the calculated value
of G at both ends, i.e., GA
and GB
and the
appropriate alignment chart.
There are two alignment charts provided by the
AISC manual,
One is for columns in braced (sidesway inhibited)
frames. See Figure C-C2.2a on page 16.1-191 ofthe AISC manual. 0 < K 1
The second is for columns in unbraced (sidesway
uninhibited) frames. See Figure C-C2.2b on page
16.1-192 of the AISC manual. 1 < K
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Inelastic Case
G is a measure of the relative flexural rigidityofthe columns (EI
c/L
c) with respect to the beams
(EIb/Lb) However, if column buckling were to occur in the
inelastic range (c
< 1.5), then the flexural rigidity
of the column will be reduced because Ic
will be
the moment of inertia of only the elastic core ofthe entire cross-section.
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rc = 10 ksi
rt = 5 ksi
rt = 5 ksi
rt = 5 ksi
rc = 10 ksi
(a) Initia l state residual st ress (b) Partially y ielded sta te at buckling
Yielded zone
Elastic core, Ic
rc = 10 ksi
rt = 5 ksi
rt = 5 ksi
rt = 5 ksi
rc = 10 ksi
rc = 10 ksi
rt = 5 ksi
rt = 5 ksi
rt = 5 ksi
rc = 10 ksi
(a) Initia l state residual st ress (b) Partially y ielded sta te at buckling
Yielded zone
Elastic core, Ic
Yielded zone
Elastic core, Ic
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Inelastic stiffness
The beams will have greater flexural rigidity
when compared with the reduced rigidity
(EIc) of the inelastic columns. As a result,
the beams will be able to restrain the
columns better, which is good for column
design.
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Inelastic Stiffness
The ratio Fcr/ Fe is called
Stiffness reduction factor
( )22
658.0877.0877.0
)658.0(
,
, 2
2
cc c
Fy
c
Fy
elasticFcr
inelasticFcr
=
=
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Procedure for Column Design
1. Design Load
2. Assume Fcr
Pn = Ag Fcr= Pu
Find Ag
Select a section
3. Find
1. Find
c = E
F
r
LK y
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Column Design
Forc
1.5 Fcr
= Fy
Forc > 1.5 Fcr = Fy
1. Fcr Calculated > Fcr Assumed
2. P > Pu. Check3. IfP > Pu, Design is OK Else Repeat
Steps 2 to 6
2c658.0
2c
877.0
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Column Design Using Design Aid
LRFD manual contains variety of Design aids,helpful in making original trial section.
1. Design load
2. Find section for Corresponding P & KL using
Column Tables in the Manual
3. Calculate an equivalent (KL)eq =
if strong axis buckling needs
checking1. Use the calculated (KL)eq value to find (cPn)
the column strength from column tables
yx
xx
r/r
LK
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Problem 4-11-1
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Solution
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THANKS