a w12x65 column section shown in the figure is pined at each end and has an additional support in the weak direction at a point 4.19m from the top. Use x = 4.71 K=1 A = 12323 rx = 134.11 ry = 76.71 Fy = 248 Determine the a) design compresive strength (KN) b.) Elastic critical buckling stress (MPa) c.) Flexural buckling stress

Engineering Fundamentals: An Introduction to Engineering (MindTap Course List)
5th Edition
ISBN:9781305084766
Author:Saeed Moaveni
Publisher:Saeed Moaveni
Chapter18: Mathematics In Engineering
Section18.6: Calculus
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a w12x65 column section shown in the figure is pined at each end and has an additional support in the weak direction at a point 4.19m from the top. Use x = 4.71 K=1

A = 12323

rx = 134.11

ry = 76.71

Fy = 248

Determine the

a) design compresive strength (KN)

b.) Elastic critical buckling stress (MPa)

c.) Flexural buckling stress

D.) Critical slenderness ratio

E.) Nominal compressive stress

F.) allowable compressive strength

 

 

 

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