Question

The relative airspeed for maximum gradient of climb is a function of engine power.

(a) True

(b) False

I got this question during a job interview.

Question is from Climb and Descent Performance with Power-Producing Engines topic in chapter Climb and Descent Performance of Aircraft Performance

Answer 1

Correct option is (a) True

For explanation: The relative airspeed for maximum gradient of climb is a function of engine power. The best climb gradient is given by u^4+λu-1=0 where u is airspeed and λ is dimensionless power.