Technical Memorandum - National Advisory Committee for Aeronautics, Volumes 1151-1160
National Advisory Committee for Aeronautics, 1947 - Aeronautics
Chiefly translations from foreign aeronautical journals.
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aerodynamics AERONAUTICS TECHNICAL MEMORANDUM airfoil angle of attack apple curves approximation aspect ratio assumed axial axis boundary condition Busemann Chaplygin COMMITTEE FOR AERONAUTICS complex potential compressibility shock computed contour corresponding deflected denote determined differential equation drop equal to zero expression Figure finite flow velocity fluid flutter formula free vortices hence holomorphic hydrodynamic forces incompressible induced drag coefficient infinitely infinity integral investigated Joukowsky profile Kehl lift coefficient lift force lifting line linear Mach number meridian curves meridian lines NACA TM NATIONAL ADVISORY COMMITTEE oblique flow oblique shock obtain origin of coordinates plane plate potential flow Prandtl reference region shock polars solution stationary straight flow stream function strophoid Strouhal subsonic SUPERSONIC FLOW Supersonic Velocities surface theory transformation unsteady motion variable vector velocity components velocity of evaporation velocity potential vortex intensity vortex wake wind tunnel wing