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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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