Structural Analysis Degree of static indeterminacy of a rigid-jointed plane frame having 15 members, 3 reaction components and 14 joints is 9 8 6 7 9 8 6 7 ANSWER DOWNLOAD EXAMIANS APP
Structural Analysis The effective length of lacing is the distance Between the inner end rivets of the bar for single lacing All of these 0.7 of the distance between the inner end rivets of the bar for double lacing Between the inner ends of effective lengths of welds connecting the members Between the inner end rivets of the bar for single lacing All of these 0.7 of the distance between the inner end rivets of the bar for double lacing Between the inner ends of effective lengths of welds connecting the members ANSWER DOWNLOAD EXAMIANS APP
Structural Analysis The slenderness effect of a wall is considered if the effective height of the wall exceeds the thickness 11 times 12 times 10 times 13 times 11 times 12 times 10 times 13 times ANSWER DOWNLOAD EXAMIANS APP
Structural Analysis The effective and actual lengths of a cantilever are same if continuous at the support, Unstrained against torsion at the support and free at the end Restrained against torsion at the support and free at the end With partial restraint against torsion of the support and free at the end None of these Unstrained against torsion at the support and free at the end Restrained against torsion at the support and free at the end With partial restraint against torsion of the support and free at the end None of these ANSWER DOWNLOAD EXAMIANS APP
Structural Analysis For a single point load W moving on a symmetrical three hinged parabolic arch of span L, the maximum sagging moment occurs at a distance x from ends. The value of x is 0.25 L 0.234 L 0.5 L 0.211 L 0.25 L 0.234 L 0.5 L 0.211 L ANSWER DOWNLOAD EXAMIANS APP
Structural Analysis For the stability of a structural part, the weight or anchorage should be 1.2 times the minimum overturning moment due to dead load Sum of (a) and (b) None of these 1.4 times the minimum overturning moment due to dead load 1.2 times the minimum overturning moment due to dead load Sum of (a) and (b) None of these 1.4 times the minimum overturning moment due to dead load ANSWER DOWNLOAD EXAMIANS APP
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