Which of the following is correct value for rate of climb if an aircraft has free stream velocity of 125 m/s? Consider steady climb at climb angle of 10°.

Which of the following is correct value for rate of climb if an aircraft has free stream velocity of 125 m/s? Consider steady climb at climb angle of 10°.

(a) 21.70 m/s

(b) 12 m

(c) 35 m/min

(d) 1.302 min/m

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I'd like to ask this question from Flight Mechanics topic in division Performance and Flight Mechanics of Aircraft Design

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Which of the following is correct value for rate of climb if an aircraft has free stream velocity of 125 m/s? Consider steady climb at climb angle of 10°.

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