Step 1: Euler's buckling formula.
The elastic buckling load for a column is:
\[
P_{cr} = \frac{\pi^2 EI}{(K L)^2}
\]
where
- $E$ = Young's modulus,
- $I$ = area moment of inertia,
- $L$ = column length,
- $K$ = effective length factor (depends on end conditions).
Step 2: Effect of flexural rigidity.
Flexural rigidity $EI$ appears in numerator. Higher $EI$ $\Rightarrow$ larger $P_{cr}$.
Thus, (A) is true.
Step 3: Effect of length.
Column length appears squared in denominator: $(KL)^2$. Larger $L$ $\Rightarrow$ smaller $P_{cr}$.
So (B) is false (load decreases, not increases).
Step 4: Effect of boundary conditions.
Boundary conditions determine $K$. For example:
- Both ends pinned: $K=1$.
- One end fixed, other free: $K=2$.
- Both ends fixed: $K=0.5$.
So end conditions strongly affect $P_{cr}$.
Thus, (C) is true.
Step 5: Effect of density.
Formula contains $E$, $I$, $L$, $K$ — no direct dependence on material density. Density matters only in self-weight buckling but not in Euler's formula.
Thus, (D) is true.
Step 6: Final check.
Correct statements are (A), (C), (D).
\[
\boxed{\text{Correct statements: (A), (C), and (D)}}
\]
A uniform symmetric cross-section cantilever beam of length \( L \) is subjected to a transverse force \( P \) at the free end, as shown in the figure. The Young’s modulus of the material is \( E \) and the moment of inertia is \( I \). Ignoring the contributions due to transverse shear, the strain energy stored in the beam is ___________.

A simply supported horizontal beam is subjected to a distributed transverse load varying linearly from \( q_0 \) at A to zero at B, as shown in the figure. Which one of the following options is correct?

Two designs A and B, shown in the figure, are proposed for a thin-walled closed section that is expected to carry only torque. Both A and B have a semi-circular nose, and are made of the same material with a wall thickness of 1 mm. With strength as the only criterion for failure, the ratio of maximum torque that B can support to the maximum torque that A can support is _________ (rounded off to two decimal places).
A thin flat plate is subjected to the following stresses: \[ \sigma_{xx} = 160 \, {MPa}; \, \sigma_{yy} = 40 \, {MPa}; \, \tau_{xy} = 80 \, {MPa}. \] Factor of safety is defined as the ratio of the yield stress to the applied stress. The yield stress of the material under uniaxial tensile load is 250 MPa. The factor of safety for the plate assuming that material failure is governed by the von Mises criterion is _________ (rounded off to two decimal places).
A prismatic vertical column of cross-section \( a \times 0.5a \) and length \( l \) is rigidly fixed at the bottom and free at the top. A compressive force \( P \) is applied along the centroidal axis at the top surface. The Young’s modulus of the material is 200 GPa and the uniaxial yield stress is 400 MPa. If the critical value of \( P \) for yielding and for buckling of the column are equal, the value of \( \frac{l}{a} \) is __________ (rounded off to one decimal place).
A uniform rigid bar of mass 3 kg is hinged at point F, and supported by a spring of stiffness \( k = 100 \, {N/m} \), as shown in the figure. The natural frequency of free vibration of the system is ___________ rad/s (answer in integer).
A jet-powered airplane is steadily climbing at a rate of 10 m/s. The air density is 0.8 kg/m³, and the thrust force is aligned with the flight path. Using the information provided in the table below, the airplane’s thrust to weight ratio is ___________ (rounded off to one decimal place). 