Yayın: Climb Performance of a Piston-Propeller Airplane with Cambered Wing and Variable Propeller Efficiency
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Anahtar kelimeler
Airplane, Climb, Propeller, Wing, Marine engineering, Piston (optics), Aerospace engineering, Aeronautics, Engineering, Wing loading, Wing configuration, Advance ratio, Angle of attack, Physics, Blade pitch, Aerodynamics, Turbine