A 5000 kg airplane is powered by an engine capable of producing
1500 kW power. Calculate the maximum angle of climb (in degrees) at
an air speed of 130 knots if the efficiency of the propeller is
80%, and the drag at this speed is 6.7 kN. Round off your answer to
the ones place. Indicate only the numeric value of your
response.
A 5000 kg airplane is powered by an engine capable of producing 1500 kW power. Calculate the maximum angle of climb (in
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answerhappygod
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A 5000 kg airplane is powered by an engine capable of producing 1500 kW power. Calculate the maximum angle of climb (in
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