Technical Memorandum - National Advisory Committee for Aeronautics, Issues 1331-1340
National Advisory Committee for Aeronautics, 1952 - Aeronautics
Chiefly translations from foreign aeronautical journals.
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AERONAUTICS TECHNICAL MEMORANDUM airfoil airplane alloys approximate assumed asymptotic Blasius Blasius boundary layer blowing slot boundary layer C.G.S. system calculation caster angle caster length Chalais-Meudon circular cylinder coefficient colors COMMITTEE FOR AERONAUTICS computed condition constant corresponding cosh curve damper defined deflection determined differential equation displacement displacement thickness divergence drift effect ejectors equation 22 experimental Figure flap flow force F formula function gives gyroscopic hence hodograph Hydrofoils increase injectors Kantrowitz kinematic shimmy lateral elasticity lift coefficient linear maximum metal NACA TM NATIONAL ADVISORY COMMITTEE oscillation oxide layer oxygen phenomenon pivot plate potential flow present theory pressure reaction product reference restoring torque shown solution speed Sretensky stagnation point stagnation pressure straight line stream function suction surface swept wing tanh temperature tests thickness tion tire torque tricycle gear turbojet values velocity viscous wave resistance wing zero