Buckling
of Columns
*Example: A slender beam (shown
below) has length, L, and modulus of elasticity, E. It but not in the
z-direction. The x-section of the beam
(shown below) is b
x h. Determine the |
Strategy: Calculate the critical load by
applying Pcr = n π2EI/L2 for buckling in the z-direction and for buckling in the
x-direction. Set them equal and solve
for h/b. Note: The critical buckling load depends on the
sizes of the moment of inertia and the The moments of inertia, I,
are as follows: Izz
= (1/12)hb3 and Ixx =
(1/12)bh3
Next consider the buckled
mode shape. The mode shape for
buckling in the z-direction is a single sine wave. Whereas the mode shape for buckling in the
x-direction, due to the restraint at mid-span, will be a
double sine wave. Click here to continue
this example. |
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