Correct answer is (a) Climb velocity
For explanation: The momentum equation for the helicopter in flight condition is given by:
T=\(\dot {m}\)(V+w)-\(\dot {m}\)V
T=\(\dot {m}\)w
Where, V is the climb velocity
w is the induced velocity in the wake region
T is the thrust
\(\dot {m}\) is mass flux
On observing the equation, we see that the momentum equation is independent of the climb velocity.