At sea-level, the total drag of an aircraft of mass 5500 kg is 5
kN at a speed of 160 knots. Calculate the rate of climb (in knots)
at an indicated air speed of 160 knots at 10000 ft, if the power
available is 980 kW and the relative air density is 0.739. Round
off your answer to the ones place. Indicate only the numeric value
of your response.
At sea-level, the total drag of an aircraft of mass 5500 kg is 5 kN at a speed of 160 knots. Calculate the rate of climb
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At sea-level, the total drag of an aircraft of mass 5500 kg is 5 kN at a speed of 160 knots. Calculate the rate of climb
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