Structural Analysis The number of independent equations to be satisfied for static equilibrium in a space structure is 7 9 6 8 7 9 6 8 ANSWER DOWNLOAD EXAMIANS APP
Structural Analysis When a load crosses a through type Pratt truss in the direction left to right, the nature of force in any diagonal member in the left half of the span would Change from compression to tension Change from tension to compression Always be compression Always be tension Change from compression to tension Change from tension to compression Always be compression Always be tension ANSWER DOWNLOAD EXAMIANS APP
Structural Analysis The Castigliano's second theorem can be used to compute deflections At the point under the load only For any type of structure For beams and frames only In statically determinate structures only At the point under the load only For any type of structure For beams and frames only In statically determinate structures only 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 0.5 L 0.25 L 0.211 L 0.234 L 0.5 L 0.25 L 0.211 L 0.234 L 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 For the stability of a structural part, the weight or anchorage should be 1.4 times the minimum overturning moment due to dead load Sum of (a) and (b) None of these 1.2 times the minimum overturning moment due to dead load 1.4 times the minimum overturning moment due to dead load Sum of (a) and (b) None of these 1.2 times the minimum overturning moment due to dead load ANSWER DOWNLOAD EXAMIANS APP
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