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Ch13 - Buckling of Columns

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86 views12 pages

Ch13 - Buckling of Columns

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백주환
Copyright
© © All Rights Reserved
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Chapter 13: Buckling of Columns

Objectives
✓ Understand the behavior of columns and concept of critical load
and buckling
✓ Determine the axial load needed to buckle a so-called ‘ideal’
column
✓ Determine the ‘effective length’ of a column with various end-
conditions

Solid Mechanics (edited by Byoung-Ho Choi) Page 1


13.1 Critical Load
• Columns: is long slender members subjected to an axial compressive
force
• Buckling: is the lateral deflection that occurs

➢ Critical Load, Pcr


• The maximum axial load that a column can support when it is on the
verge of buckling is called the critical load.

Solid Mechanics (edited by Byoung-Ho Choi) Page 2


13.1 Critical Load

• From the free-body diagram: kL


2 P tan  = F = k   = k (L / 2) • Stable equilibrium : P 
4
• For small θ, tan θ ≈ θ,
kL
2 P = k (L / 2 ) • Unstable equilibrium : P 
4
P = kL / 4 (independent of  )

Solid Mechanics (edited by Byoung-Ho Choi) Page 3


13.2 Ideal Column with Pin Supports
➢ Ideal Column
• It is perfectly straight before loading
• Both ends are pin-supported
• Loads are applied throughout the centroid of the cross section

Solid Mechanics (edited by Byoung-Ho Choi) Page 4


13.2 Ideal Column with Pin Supports

• Some slender pin-connected


members used in moving
machinery, such as this short
link, are subjected to
compressive loads and thus
act as columns.

• Typical interior steel pipe


columns used to support the
roof of a single story building.

Solid Mechanics (edited by Byoung-Ho Choi) Page 5


13.2 Ideal Column with Pin Supports
➢ Behavior
• When P < Pcr, the column remains straight.
• When P = Pcr,
d 2v
EI 2 = M = − Pv
dx
d 2v  P 
+  v = 0
dx 2  EI 
 P   P 
v = C1 sin  x  + C2 cos x 
 EI   EI 
• Since v=0 at x=0, then C2 = 0
 P 
• Since v=0 at x=L, then 1  C sin L  = 0
 EI 
 P 
• Therefore, sin  L  = 0
 EI 
 P 
• Which is satisfied if sin  L  = n
 EI 
n 2 2 EI
• Or P = L2 where n = 1,2,3,...
Solid Mechanics (edited by Byoung-Ho Choi) Page 6
13.2 Ideal Column with Pin Supports

• A column will buckle about the principal axis of the cross section having
the least moment of inertia.

• A column having a rectangular cross section,


like a meter stick, as shown in Fig. 13-6,
will buckle about the a-a axis, not the b-b axis.

Solid Mechanics (edited by Byoung-Ho Choi) Page 7


13.2 Ideal Column with Pin Supports

 2 EI
• Smallest value at P is when n=1, thus Pcr =
L2
 2E
• Corresponding stress is  cr =
(KL / r )2
• Where r = I / A is called ‘radius of gyration’

• (L/r) is called the ‘slenderness ratio.’

• The critical-stress curves are hyperbolic,

valid only for σcr is below yield stress

Solid Mechanics (edited by Byoung-Ho Choi) Page 8


13.3 Columns Having Various Types of
Supports

• The tubular columns used to support


this water tank have been braced at
three locations along their length to
prevent them from buckling.

Solid Mechanics (edited by Byoung-Ho Choi) Page 9


13.3 Columns Having Various Types of
Supports
➢ Columns having various end-conditions
• Consider the moment-deflection equation for the cantilevered column,
which is fixed at the base.
d 2v
EI 2 = P( − v )
dx
P
EIV + 2 v = 2 where 2 =
EI
• The solution is v = C1 sin (x ) + C2 cos(x ) + 

• Since v = 0 at x = 0, so that C2 = −

• Also, v' = C1 cos(x ) − C2  sin (x )

• Since v’ = 0 at x = 0, so that C1 = 0

Solid Mechanics (edited by Byoung-Ho Choi) Page 10


13.3 Columns Having Various Types of
Supports

• Hence v =  1 − cos(x )x = 0

• Since v = δ at x = L, thus
 cos(L ) = 0
n
 cos(L ) = 0 or L =
2
• The smallest critical load occurs when n = 1, thus
 2 EI  2 EI
Pcr = or Pcr = (with K = 2)
4L 2
(KL )2

• K is called the ‘effective-length factor’

Solid Mechanics (edited by Byoung-Ho Choi) Page 11


13.3 Columns Having Various Types of
Supports
➢ Specific values of K

Solid Mechanics (edited by Byoung-Ho Choi) Page 12

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