Find the critical load of the column F-G: perform the stability analysis for column F - G in figure 4, given that it is a 1/8" X 3/4" section and is 1m long. The dimensions of the assembly are: E - G = 1.135 m and EF = 0.725 m. [Column F-G is aluminum] E LLV 0 im W G

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Buckling
Find the critical load of the column F-G:
perform the stability analysis for column F-
G in figure 4, given that it is a 1/8" X 3/4"
section and is 1m long. The dimensions of
the assembly are: E - G = 1.135 m and EF
= 0.725 m. [Column F-G is aluminum]
E
LLV
0
im
W
G
Transcribed Image Text:Buckling Find the critical load of the column F-G: perform the stability analysis for column F- G in figure 4, given that it is a 1/8" X 3/4" section and is 1m long. The dimensions of the assembly are: E - G = 1.135 m and EF = 0.725 m. [Column F-G is aluminum] E LLV 0 im W G
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