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THE ANATOMY OF THE AIRPLANE
THEORY AND EXPERIMENTWIND TUNNELS
16 other sections not shown
aerodynamic Aeronautics airfoil airplane airspeed ambient angle of attack assumed blade body Boeing boundary layer camber chord climb constant control surface Courtesy cruise curve cylinder decrease density distance downwash drag coefficient drag due effect equation equivalent airspeed field length fighter flap flight path flow fluid flying force freestream ft/s fuselage gradient higher incompressible increase induced drag laminar leading edge lift coefficient lift per square load factor lower surface Mach number Mach wave minimum nacelles parasite drag planform pressure altitude propeller propulsive reduced result Reynolds number rocket sea level shown in Figure skin friction speed of sound stability stall static streamlines structural subsonic supersonic sweepback swept wing takeoff temperature test section thickness ratio thrust total pressure trailing edge transport aircraft turbofan turboprop upper surface velocity viscosity vortex vortices wave drag weight wind tunnel wing area zero