4 pages matching singleâ€”rotation propeller in this book
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88 airplane Advance Restricted Report adverse yaw aileron rolls airfoil airspeed Figure Ames Aeronautical Laboratory angle of attack boundary layer calculated characteristics chord circular cylinder COMMITTEE FOR AERONAUTICS Comparison between flight compressible flow Compressible Fluids computed curves downwash dual—rotation propeller dynamic pressure effects of power experimental flaps flight determinations free stream heat transfer heat-transfer coefficient hoat ion propeller laminar boundary layer lateral stability Left Total aileron lift coefficient Mach number maximum rolling velocity Moffett Field NACA NATIONAL ADVISORY COMMITTEE normal rated power P-61A airplane peller percent take—off power pressure coefficient PV-1 airplane rate of heat reference rolls from straight rosult shown sideslip angle single—rotat ion single—rotation propeller skin slipstream straight flight streamline body temperature difference tests thrust coefficient tion Total aileron deflection turning flight unbanked flight values variation velocity potential vertical surface WARTIME REPORT ORIGINALLY wing zero yaw