Structural Analysis Degree of kinematic indeterminacy of a pin-jointed plane frame is given by 2j + r 3j – r j – 2r 2j – r 2j + r 3j – r j – 2r 2j – r ANSWER DOWNLOAD EXAMIANS APP
Structural Analysis A pin-jointed plane frame is unstable if (where m is number of members, r is reaction components and j is number of joints) (m + r)>2j (m + r)<2j None of these m + r = 2j (m + r)>2j (m + r)<2j None of these m + r = 2j 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 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 the head of the load reaches the section ANSWER DOWNLOAD EXAMIANS APP
Structural Analysis Muller Breslau’s principle for obtaining influence lines is applicable to i) trusses ii) statically determinate beams and frames iii) statically indeterminate structures, the material of which is elastic and follows Hooke’s law iv) any statically indeterminate structure The correct answer is (i) and (ii) (i), (ii) and (iii) only (i) (i), (ii) and (iv) (i) and (ii) (i), (ii) and (iii) only (i) (i), (ii) and (iv) ANSWER DOWNLOAD EXAMIANS APP
Structural Analysis For the stability of a structural part, the weight or anchorage should be Sum of (a) and (b) 1.2 times the minimum overturning moment due to dead load None of these 1.4 times the minimum overturning moment due to dead load Sum of (a) and (b) 1.2 times the minimum overturning moment due to dead load None of these 1.4 times the minimum overturning moment due to dead load ANSWER DOWNLOAD EXAMIANS APP
Structural Analysis When a series of wheel loads crosses a simply supported girder, the maximum bending moment under any given wheel load occurs when The wheel load under consideration is midway between the centre of span and the centre of gravity of the load system The centre of span is midway between the centre of gravity of the load system and the wheel load under consideration None of these The centre of gravity of the load system is midway between the centre of span and wheel load under consi-deration The wheel load under consideration is midway between the centre of span and the centre of gravity of the load system The centre of span is midway between the centre of gravity of the load system and the wheel load under consideration None of these The centre of gravity of the load system is midway between the centre of span and wheel load under consi-deration ANSWER DOWNLOAD EXAMIANS APP
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