Step 1: Analyze A.
"Plane section remains plane before and after bending" is the fundamental assumption of bending theory (Bernoulli's assumption). It gives linear strain distribution. So, A → II.
Step 2: Analyze B.
"Material is elastic and deflections are small" implies elastic analysis where superposition holds good. Hence, B → I.
Step 3: Analyze C.
"Uniqueness theorem" ensures a unique solution in structural analysis, applied in non-linear stability/buckling problems. Thus, C → III.
Step 4: Analyze D.
"Large deformation" concept is used in plastic analysis to determine the collapse load. So, D → IV.
Step 5: Conclusion.
The correct matching is:
\[
A - II, B - I, C - III, D - IV
\]
The solution(s) of the ordinary differential equation $y'' + y = 0$, is:
(A) $\cos x$
(B) $\sin x$
(C) $1 + \cos x$
(D) $1 + \sin x$
Choose the most appropriate answer from the options given below:
For the matrix, $A = \begin{bmatrix} -4 & 0 \\ -1.6 & 4 \end{bmatrix}$, the eigenvalues ($\lambda$) and eigenvectors ($X$) respectively are:
The value of $\iint_S \vec{F} \cdot \vec{N} \, ds$ where $\vec{F} = 2x^2y \hat{i} - y^2 \hat{j} + 4xz^2 \hat{k}$ and $S$ is the closed surface of the region in the first octant bounded by the cylinder $y^2 + z^2 = 9$ and the planes $x = 0, x = 2, y = 0, z = 0$, is:
The value of the integral $\displaystyle \oint_C \frac{z^3 - 6}{2z - i} \, dz$, where $C: |z| \leq 1$, is:
For the frame shown in the figure below, the maximum moment in the left column shall be (Assuming Moment of Inertia (I) of all the members is same):
