Structural Analysis A load W is moving from left to right support on a simply supported beam of span T. The maximum bending moment at 0.4 1 from the left support is 0.24 Wl 0.20 Wl 0.16 Wl 0.25 Wl 0.24 Wl 0.20 Wl 0.16 Wl 0.25 Wl ANSWER DOWNLOAD EXAMIANS APP
Structural Analysis The thickness of the rectangular plate for the cap or base of a solid round steel columns, is calculated from the formulat = √[(9W/16 fbct) × D/(D -d)] where ‘d’ is The reduced diameter of the column The dimension of the base The diameter of the base The diameter of the top The reduced diameter of the column The dimension of the base The diameter of the base The diameter of the top 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 -3 mm to +3 mm -2 mm to +2 mm -5 mm to +5 mm -4 mm to +4 mm -3 mm to +3 mm -2 mm to +2 mm -5 mm to +5 mm -4 mm to +4 mm 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 0.211 L 0.5 L 0.234 L 0.25 L 0.211 L 0.5 L 0.234 L 0.25 L 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 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 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 ANSWER DOWNLOAD EXAMIANS APP
Structural Analysis For the stability of a structural part, the weight or anchorage should be 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 None of these 1.2 times the minimum overturning moment due to dead load Sum of (a) and (b) ANSWER DOWNLOAD EXAMIANS APP
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