Structural Analysis To generate the j th column of the flexibility matrix a unit displacement is applied at co-ordinate j and the forces are calculated at all coordinates a unit force is applied at coordinate j and the forces are calculated at all coordinates a unit force is applied at coordinate j and the displacements are calculated at all coordinates a unit displacement is applied at co-ordinate j and the displacements are calculated at all co-ordinates a unit displacement is applied at co-ordinate j and the forces are calculated at all coordinates a unit force is applied at coordinate j and the forces are calculated at all coordinates a unit force is applied at coordinate j and the displacements are calculated at all coordinates a unit displacement is applied at co-ordinate j and the displacements are calculated at all co-ordinates ANSWER DOWNLOAD EXAMIANS APP
Structural Analysis The degree of kinematic indeterminacy of a pin-jointed space frame is (where m, r and j have their usual meanings) j-3r 2j-r 3j-r j-2r j-3r 2j-r 3j-r j-2r ANSWER DOWNLOAD EXAMIANS APP
Structural Analysis In the displacement method of structural analysis, the basic unknowns are displacements and forces displacements None of these force displacements and forces displacements None of these force ANSWER DOWNLOAD EXAMIANS APP
Structural Analysis If the specified thickness of a footing is 100 cm, the depth of the form work may be tolerated from -4 mm to +4 mm -5 mm to +5 mm -3 mm to +3 mm -2 mm to +2 mm -4 mm to +4 mm -5 mm to +5 mm -3 mm to +3 mm -2 mm to +2 mm ANSWER DOWNLOAD EXAMIANS APP
Structural Analysis When a uniformly distributed load, longer than the span of the girder, moves from left to right, then the maximum bending moment at mid section of span occurs when the uniformly distributed load occupies Less than the left half span Whole span More than the left half span Whole of left half span Less than the left half span Whole span More than the left half span Whole of left half span ANSWER DOWNLOAD EXAMIANS APP
Structural Analysis For the stability of a structural part, the weight or anchorage should be None of these 1.2 times the minimum overturning moment due to dead load Sum of (a) and (b) 1.4 times the minimum overturning moment due to dead load None of these 1.2 times the minimum overturning moment due to dead load Sum of (a) and (b) 1.4 times the minimum overturning moment due to dead load ANSWER DOWNLOAD EXAMIANS APP
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