The correct answer is (a) 10.046 kN-m
For explanation: Given : R = 50 m ; v = 200 km/hr = 55.6 m/s ; m = 400 kg ; k = 0.3 m ;
N = 2400 r.p.m. or ω = 2π × 2400/60 = 251 rad/s
We know that mass moment of inertia of the engine and the propeller,
I = mk^2 = 36 kg-m^2
and angular velocity of precession,
ωP = v/R = 55.6/50 = 1.11 rad/s
We know that gyroscopic couple acting on the aircraft,
C = I. ω. ωP = 36 × 251.4 × 1.11 = 100 46 N-m
= 10.046 kN-m