Внутрішня аеродинаміка/ Внутренняя аэродинамика/Internal aerodynamics
Підтеми:
- Внутрішня аеродинаміка впускних отворів, повітрозабирачів/Внутренняя аэродинамика воздухозаборников и выходных устройств/Air inlets and output devices
- Внутрішня аеродинаміка сопел, форсунок/Внутренняя аэродинамика сопол, форсунок/Nozzles
- Внутрішня аеродинаміка тіл в каналах/Внутренняя аэродинамика тел в каналах/Bodies in channels
- Внутрішня аеродинаміка каналів, колін, відводів, дифузорів, вихрових трубок/Каналы. Колена. Отводы. Дроссели. Вихревые трубки. Диффузоры/Channels. Knee. Branches. Throttles. Vortex tubes. Diffuzora
- Внутрішня аеродинаміка ежекторів, струменевих насосів, вихідних пристроїв, випускних отворів/Внутренняя аэродинамика эжекторов, струйных насосов, выходных устройств/Ejectors. Jet pumps. Output devices
Документи:
- A Thermodynamic Study of the Turbine - Propeller Engine [Текст] : Report / National Advisory Committee For Aeronautics. — Washington : U.S. Government Printing Office, 1953. — 36 p.
- A Wind - Tunnel Test Technique for Measuring the Dynamic Rotary Stability Derivatives at Subsonic and Supersonic Speeds [Текст] : Report / NACA. — Washington : U.S. Government Printing Office, 1956. — 14 p.
- Cопряженное численное моделирование внутренней и внешней аэродинамики системы двигатель - корпус летательного аппарата [Текст] / Ю.П. Кухтин, В.М. Лапотко, А.В. Еланский // Авиационно-космическая техника и технология : Научно-технический журнал. — Х. : Нац. аэрокосмический ун-т "ХАИ", 2014. — С. 21-26.
- Calculated and Measured Stresses in Simple Panels Subject to Intense Random Acoustic Loading Including the Near Noise Field of a Turbojet Engine [Текст] : Report / NACA. — Washington : U.S. Government Printing Office, 1958. — 10 p.
- Effect of Fuel Variables on Carbon Formation in Turbojet-Engine Combustors [Текст] : Report / NACA. — Washington : U.S. Government Printing Office, 1958. — 18 p.
- Experimental and Theoretical Studies of Axisimmetric Free Jets [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1959. — 292 p.
- Extrapolation Tehniques Applied to Matrix Methods in Neutron Diffusion Problems [Текст] : Report / NACA. — Washington : U.S. Government Printing Office, 1956. — 10 p.
- Factors that Affect Operational Reliability of Turbojet Engines [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1960. — 211 p.
- Fast Interplanetary Missions With Low-Thrust Propulsion System [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1961. — 29 p.
- Flight Determination of Drag of Normal-Shock Nose Inlets With Various Cowling Profiles at Mach Numbers From 0.9 to 1.5 [Текст] : Report / NACA. — Washington : U.S. Government Printing Office, 1956. — 19 p.
- Ground Reflaction of Jet Noise [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1959. — 29 p.
- Ground Simulator Studies of the Effects of Valve Friction, Stic Friction, Flexibility, and Backlash on Power Control System Quality [Текст] : Report / NACA. — Washington : U.S. Government Printing Office, 1958. — 13 p.
- Growth of Disturbances in a Flame-Generated Shear Region [Текст] : Report / NACA. — Washington : U.S. Government Printing Office, 1958. — 46 p.
- Investigation of the Aerodynamic Characteristics of a Model Wing - Propeller Combination and of the Wing and Propeller Separately at Angles of Attack up to 90 [Текст] : Report / NACA. — Washington : U.S. Government Printing Office, 1956. — 40 p.
- Jet-Boundary Corrections for Lifting Rotors Centered in Rectangular Wind Tunnels [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1960. — 62 p.
- Linearized Theory of Wind-Tunnel Jet-Boundary Corrections and Ground Effect for VTOL-STOL Aircraft [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1962. — 269 p.
- NACA Investigation of Fuel Performance in Piston-Type Engines [Текст] : Report / National Advisory Committee for Aeronautics. — Washington : U.S. Gowernment Printing Office, 1951. — 192 p.
- NACA Research on Slurry Fuels [Текст] : Report / NACA. — Washington : U.S. Government Printing Office, 1958. — 24 p.
- Numerical Predictions of Radiative Interchange Between Conducting Fins with Mutual Irradiations [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1961. — 22 p.
- On Boattail Bodies of Revolution Having Minimum Wave Drag [Текст] : Report / NACA. — Washington : U.S. Government Printing Office, 1956. — 9 p.
- Origin and Prevention of Crash Fires in Turbojet Aircraft [Текст] : Report / NACA. — Washington : U.S. Government Printing Office, 1958. — 19 p.
- Photographic Investigation of Combustion in a Two - Dimentional Transparent Rocket Engine [Текст] : Report / National Advisory Committee For Aeronautics. — Washington : U.S. Government Printing Office, 1953. — 12 p.
- Physical Measurements in Gas Dynamics and Combustion [Текст]. — Princeton, New Jersey : Princeton University Press, 1954. — 578 p.
- Propellant Vaporization as a Design Criterion for Rocket-Engine Combustion Chambers [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1960. — 55 p.
- Reciprocity Relations in Aerodynamics [Текст] : Report / National Advisory Committee For Aeronautics. — Washington : U.S. Government Printing Office, 1953. — 16 p.
- Similarity of Far Noise Fields of Jets [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1960. — 44 p.
- Similarity of Near Noise Fields of Subsonic Jets [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1961. — 54 p.
- Spectra and Diffusion in a Round Turbulent Jet [Текст] : Report / National Advisory Committee for Aeronautics. — Washington : U.S. Gowernment Printing Office, 1951. — 21 p.
- Survey of Hydrogen Combution Properties [Текст] : Report / NACA. — Washington : U.S. Government Printing Office, 1958. — 34 p.
- Systematic Two-Dimentional Cascade Tests of NACA 65-Series Compressor Blades at Low Speeds [Текст] : Report / NACA. — Washington : U.S. Government Printing Office, 1958. — 85 p.
- Technikal Report of the Aeronautical Research Committee for the Year 1923-1924 (With Appendices) [Текст] : Scale Effects, Materials, Compasses, Engines, &c. — London : Majesty's Stationery Office, 1925. — 682 p.
- Technikal Report of the Aeronautical Research Committee for the Year 1930-1931 (With Appendices) [Текст] : Stability and Control, Engines, etc. — London : Majesty's Stationery Office, 1932. — 912 p.
- Technikal Report of the Aeronautical Research Committee for the Year 1934-1935 [Текст] : . Seaplanes, Stuctures, Engines, Materials, etc. — London : Majesty's Stationery Office, 1936. — 1144 p.
- Technikal Report of the Aeronautical Research Committee for the Year 1935-1936 [Текст] : Stuctures, Flutter, Engines, Seaplanes, etc. — London : Majesty's Stationery Office, 1937. — 762 p.
- The Near Noise Field of Static Jets and Some Model Studies of Devices for Noise Reduction [Текст] : Report / NACA. — Washington : U.S. Government Printing Office, 1956. — 12 p.
- Theoretical Analysis of Total-Pressure Loss and Airflow Distribution For Turbular Turbojet Combustors With Constant Annulus and Liner Cross-Sectional Areas [Текст] : Report / NACA. — Washington : U.S. Government Printing Office, 1958. — 26 p.
- Theoretical Combution Perfomance of Several High-Energy Fuels for Ramjet Engines [Текст] : Report / NACA. — Washington : U.S. Government Printing Office, 1958. — 18 p.
- Theoretical Perfomance of Hydrogen-Oxygen Rocket Thrust Chambers [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1961. — 75 p.
- Theory of Self-Excited Mechanical Oscillations of Helicopter Rotors With Hinged Blades [Текст] : Report / NACA. — Washington : U.S. Government Printing Office, 1958. — 39 p.
- Two-Dimentional Diffusion Theory Analysis of Reactivity Effects of a Fuel-Plate-Removal Experiment [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1959. — 15 p.
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