Течія з надзвуковими швидкостями (М від 1,0 до 4,99)/Течение при сверхзвуковых скоростях (М от 1,0 до 4,99)/Flow at supersonic speeds (M 1.0 to 4.99)
Підтеми:
Документи:
- Jet Effects on Annular Base Pressure and Temperature in a Supersonic Stream [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1962. — 40 p.
- Laminar Boundry Layer on Cone in Supersonic Flow at Large Angle of Attack [Текст] : Report / National Advisory Committee For Aeronautics. — Washington : U.S. Government Printing Office, 1953. — 13 p.
- Les Souffleries Aerodynamiques a Grandes Vitesses [Текст] / J. Villey. — Paris : Ed. Blondel La Rougery, 1943. — 160 p.
- Linearized Supersonic Nonequilibrium Flow Past an Arbitrary Boundary [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1961. — 16 p.
- Linearized Theory of Steady High-Speed Flow [Текст] / G.N. Ward. — Cambridge : At the University Press, 1955. — 243 p.
- Method and Graphs for the Evaluation of Air - Induction Systems [Текст] : Report / National Advisory Committee For Aeronautics. — Washington : U.S. Government Printing Office, 1953. — 22 p.
- Minimum - Drag Ducted and Pointed Bodies of Revolution Based on Linearized Supersonic Theory [Текст] : Report / National Advisory Committee for Aeronautics. — Washington : U.S. Government Printing Office, 1955. — 9 p.
- Modern Developments in Fluid Dynamics High Speed Flow [Текст] / Howarth(edit);Fluid Motion Sub - Cmmittee of the Aeronautical Research Council. — Oxford : At the Clarendon Press, 1953. — 475 p.
- On the Application of Transonic Similarity Rules to Wings of Finite Span [Текст] : Report / National Advisory Committee for Aeronautics. — Washington : U.S. Government Printing Office, 1953. — 21 p.
- On the Kernel Function of the Integral Equation Relaying Lift and Downwash Distributions of Oscillating Wings in Supersonic Flow [Текст] : Report / NACA. — Washington : U.S. Government Printing Office, 1956. — 18 p.
- Quasi - Cylindrical Theory of Wing - Body Interference at Supersonic Speeds and Comparison With Experiment [Текст] : Report / National Advisory Committee for Aeronautics. — Washington : U.S. Government Printing Office, 1955. — 56 p.
- Several Methods for Aerodynamic Reduction of Static-Pressure Sensing Errors for Aircraft at Subsonic, Near-Sonic, and Low Supersonic Speeds [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1959. — 23 p.
- Slender-Body Theory Based on Approximate Solution of the Transonic Flow Equation [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1959. — 54 p.
- Stabilization of bluntnose cavity flows [Текст] / Национальный аэрокосмический университет им. Н.Е.Жуковского "ХАИ", г.Харьков, Украина // Аэрогидродинамика: проблемы и перспективы. Вып. 2 ; М-во образования и науки Украины, Нац. аэрокосм. ун-т им. Н. Е. Жуковского "Харьк. авиац. ин-т" - Х. : Нац. аэрокосм. ун-т им. Н. Е. Жуковского "Харьк. авиац. ин-т" , 2006. — С. 30-39.
- Supersonic Aerodynamics [Текст] / E.R.C. Miles. — New York : McGraw-Hill Book Company, Inc., 1950. — 255 p.
- Supersonic Flow Around Circular Cones at Angels of Attack [Текст] : Report / National Advisory Committee For Aeronautics. — Washington : U.S. Government Printing Office, 1951. — 11 p.
- Supersonic Flow Past a Family of Blunt Axisymmetric Bodies [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1959. — 25 p.
- Supersonic Flow Past Bodies of Revolution [Текст] / Ministry Of Supply. — London : His Majesty's Stationery Office, 1945. — 24 p.
- Theoretical Antisymmetric Span Loading for Wings of Arbitrary Plan Form at Subsonic Speeds [Текст] : Report / National Advisory Committee for Aeronautics. — Washington : U.S. Gowernment Printing Office, 1951. — 36 p.
- Theoretical Investigation of Flutter of Two-Dimentional Flat Panels With One Surface Exposed to Supersonic Potential Flow [Текст] : Report / NACA. — Washington : U.S. Government Printing Office, 1956. — 24 p.
- Theory of Wing-Body Drag at Supersonic Speeds [Текст] : Report / NACA. — Washington : U.S. Government Printing Office, 1956. — 7 p.
- The Proper Combination of Lift Loadings for Least Drag on a Supersonic Wing [Текст] : Report / NACA. — Washington : U.S. Government Printing Office, 1956. — 9 p.
- Thin Airfoil Theory Based on Approximate Solution of the Transonic Flow Equation [Текст] : Report / NACA. — Washington : U.S. Government Printing Office, 1958. — 37 p.
- Turbulent Boundary Layer on a Yawed Cone in a Supersonic Stream [Текст] : Report / NASA. — Washington : U.S. Government Printing Office, 1959. — 16 p.
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