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What is Subsonic Aerodynamics Rate of Climb about?

1) This document contains data from an experiment measuring the rate of climb of an aircraft at various speeds and altitudes. 2) The data includes lift, drag, power required, and rate of climb values for airspeeds ranging from 50 to 200 knots at sea level and 7,500 feet. 3) A graph of the power required and rate of climb data shows that the maximum rate of climb was achieved at around 150 knots at sea level and 125 knots at 7,500 feet.

Author

kloyied

Language

EN