Aerodynamics

aero aerodynamic Aeronautical aileron aircraft airfoil airplane altitude angle of attack aspect ratio assumed bird bird flight blade body boundary layer calculated called Chapter circulation component compressible consider control surface cross section curve decrease deflection density device direction drag coefficient dynamic effect engine example experimental flat plate flight flow pattern fluid mechanics flying force acting Guggenheim Aeronautics Laboratory increase induced drag Joukowski Kármán laminar Lanchester lift coefficient linearized Mach number mathematical method moving N.A.C.A. Report Newton's oscillation perpendicular phugoid Prandtl pressure rise problem produced propeller propulsion relative result Reynolds number rocket rotation shock wave skin friction sonic sound velocity span stability stall stream streamlines subsonic supersonic supersonic speed sustentation sweepback tail theoretical theory of lift thrust tion trailing edge transonic turbine turbojet turbulent flow viscosity vortex vortices wake drag weight wind tunnel wing loading wing section wing surface wing theory