An airplane with a wing loading of 2.4 kN/m2, and a
mass of 4500 kg, has a maximum thrust of 30 kN at sea-level. If the
drag coefficient at a speed of 270 knots is 0.04, find the rate of
climb in knots. Round off your answer to the ones place. Indicate
only the numeric value of your response.
An airplane with a wing loading of 2.4 kN/m2, and a mass of 4500 kg, has a maximum thrust of 30 kN at sea-level. If the
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An airplane with a wing loading of 2.4 kN/m2, and a mass of 4500 kg, has a maximum thrust of 30 kN at sea-level. If the
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