Structural Analysis The number of independent displacement components at each joint of a rigid-jointed space frame is 3 2 6 1 3 2 6 1 ANSWER DOWNLOAD EXAMIANS APP
Structural Analysis Study the following statements. i) The displacement method is more useful when degree of kinematic indeterminacy is greater than the degree of static indeterminacy. ii) The displacement method is more useful when degree of kinematic indeterminacy is less than the degree of static indeterminacy. iii) The force method is more useful when degree of static indeterminacy is greater than the degree of kinematic indeterminacy. iv) The force method is more useful when degree of static indeterminacy is less than the degree of kinematic indeterminacy. The correct answer is (ii) and (iv) (i) and (iii) (i) and (iv) (ii) and (iii) (ii) and (iv) (i) and (iii) (i) and (iv) (ii) and (iii) ANSWER DOWNLOAD EXAMIANS APP
Structural Analysis The effective length of lacing is the distance 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 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 ANSWER DOWNLOAD EXAMIANS APP
Structural Analysis When a uniformly distributed load, shorter than the span of the girder, moves from left to right, then the conditions for maximum bending moment at a section is that the head of the load reaches the section the load position should be such that the section divides the load in the same ratio as it divides the span the tail of the load reaches the section the load position should be such that the section divides it equally on both sides the head of the load reaches the section the load position should be such that the section divides the load in the same ratio as it divides the span the tail of the load reaches the section the load position should be such that the section divides it equally on both sides ANSWER DOWNLOAD EXAMIANS APP
Structural Analysis Muller Breslau’s principle for obtaining influence lines is applicable toi) trussesii) statically determinate beams and framesiii) statically indeterminate structures, the material of which is elastic and follows Hooke’s lawiv) any statically indeterminate structureThe correct answer is only (i) (i), (ii) and (iii) (i), (ii) and (iv) (i) and (ii) only (i) (i), (ii) and (iii) (i), (ii) and (iv) (i) and (ii) ANSWER DOWNLOAD EXAMIANS APP
Structural Analysis For the stability of a structural part, the weight or anchorage should be 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 1.2 times the minimum overturning moment due to dead load ANSWER DOWNLOAD EXAMIANS APP
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