A piston-powered airplane of mass m = 1000 kg is performing an quilibrium c...
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A piston-powered airplane of mass m = 1000 kg is performing an quilibrium climb at a speed v = 220 Kt. What will the ascent angle be if drag power is Pr = 115 kW, and engine power is Pa = 235 kW assuming the pilot does what it takes to keep the speed constant?
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