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?
