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Q: For the built-up shape shown in Figure, assume that the components of the cross section are connected in such a way that the section is fully effective. Fy = 50 ksi. 1- Compute A, Iy, ly, rx and ry. 2- Compute K,, Ky, Ly and Ly 3- Compute the nominal compressive strength based on flexural buckling only (Do not check local buckling). 1" x 18" 13' 1"x16" 26' 13' 1" x 18" Support in strong Support in weak direction direction

Q: For the built-up shape shown in Figure, assume that the components of the cross section are connected in such a way that the section is fully effective. Fy = 50 ksi. 1- Compute A, Iy, ly, rx and ry. 2- Compute K,, Ky, Ly and Ly 3- Compute the nominal compressive strength based on flexural buckling only (Do not check local buckling). 1" x 18" 13' 1"x16" 26' 13' 1" x 18" Support in strong Support in weak direction direction

Structural Analysis
Structural Analysis
6th Edition
ISBN:9781337630931
Author:KASSIMALI, Aslam.
Publisher:KASSIMALI, Aslam.
Chapter2: Loads On Structures
Section: Chapter Questions
Problem 1P
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Q: For the built-up shape shown in Figure, assume that the components of the cross section are connected in such a way that the section is fully effective. Fy = 50 ksi. 1- Compute A, Ix, ly, rx and ry. 2- Compute K, Ky, Ly and Ly 3. Compute the nominal compressive strength based on flexural buckling only (Do not check local buckling). 1" x 18" 13' 1"x16" 26' 13' ."18 x"נ Support in strong Support in weak direction direction
Transcribed Image Text:Q: For the built-up shape shown in Figure, assume that the components of the cross section are connected in such a way that the section is fully effective. Fy = 50 ksi. 1- Compute A, Ix, ly, rx and ry. 2- Compute K, Ky, Ly and Ly 3. Compute the nominal compressive strength based on flexural buckling only (Do not check local buckling). 1" x 18" 13' 1"x16" 26' 13' ."18 x"נ Support in strong Support in weak direction direction
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