Step 1: Structural role of ribs.
In semi–monocoque construction, the load–carrying structure consists of skin, stringers, spars, and ribs.
- Spars carry primary bending.
- Stringers carry axial stresses and resist column buckling.
- Ribs are transverse frames: they shape the airfoil, support the skin, and tie the stringers/spars.
Step 2: Assess each statement.
(A) Incorrect: Even in a rectangular planform, ribs at root and tip may differ (thickness, cutouts, taper for systems). So rib dimensions do depend on spanwise position.
(B) True: By tying longitudinal stiffeners (stringers), ribs shorten their effective column length, raising their critical buckling stress.
(C) True: Ribs subdivide skin panels into smaller effective spans, thereby raising skin plate buckling stress.
(D) True: Ribs enforce the wing's aerodynamic contour (airfoil shape), preventing distortion under load.
Final Answer:
\[
\boxed{(B),\ (C),\ (D)}
\]
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?
