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What is Maximum Rate of Climb Analysis about?

1) To climb, an aircraft must increase its potential energy by either increasing thrust or reducing drag to allow excess thrust. 2) The angle of climb is related to the difference between thrust available and thrust required divided by weight. Rate of climb can be determined using excess thrust and aircraft parameters. 3) Both angle and rate of climb can be determined graphically using thrust and drag curves or analytically using equations that relate climb to thrust, drag, weight and airspeed. The maximum

Author
Charudutt Ghormade
Language
EN