Aerospace Engineering > GATE 2014 > Aircraft Performance
Data for a light, single-engine, propeller driven aircraft in steady level flight at sea-level is as follows: velocity V∞=40m/s, weight W=13000N, lift coefficient CL=0.65, drag coefficient CD= 0.025+0.04CL2 and power available Pav=100,000J/s. The rate of climb possible for this his aircraft under the given conditions (in m/s) is
Correct : b
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