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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°.(a) 21.70 m/s(b) 12 m(c) 35 m/min(d) 1.302 min/mI got this question during an internship interview.I'd like to ask this question from Flight Mechanics topic in division Performance and Flight Mechanics of Aircraft Design

Answer» CORRECT option is (a) 21.70 m/s

Explanation: RATE of CLIMB = free stream velocity*sine (climb ANGLE) = 125*sin (10) = 21.70 m/s.


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