Теплообмін між рухомими тілами та газами. Аеротермодинаміка/Теплообмен между движущимися телами и газами. Аэротермодинамика/The heat transfer between moving bodies and gases. Aerothermodynamics
Документи:
- Boundary-Layer Similar Solutions and Correlation Equations for Laminar Heat-Transfer Distribution in Equilibrium Air at Velocities up to 41.100 Feet Per Second [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1961. — 57 p.
- Boundary-Layer Stability Diagrams for Electrically Conducting Fluids in the Presence of a Magnetic Field [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1959. — 16 p.
- Calculations of Laminar Heat Transfer Around Cylinders of Arbitrary Cross Section and Transpiration to Turbine Blade Cooling [Текст] : Report / National Advisory Committee For Aeronautics. — Washington : U.S. Government Printing Office, 1955. — 21 p.
- Comparison of Theoretical and Experimental Heat-Transfer Characteristics of Bodies of Revolution at Supersonic Speeds [Текст] : Report / National Advisory Committee for Aeronautics. — Washington : U.S. Gowernment Printing Office, 1951. — 15 p.
- Effect of Large-Amplitude Oscillations on Heat Transfer [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1962. — 24 p.
- Estimated Viscosities and Thermal Conductivities of Gases at High Temperatures [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1962. — 120 p.
- Experimental Investigation of Freeconvection Heat Transfer in Vertical Tube at large Grashof Numbers [Текст] : Report / National Advisory Committee for Aeronautics. — Washington : U.S. Government Printing Office, 1955. — 14 p.
- Fluid Dynamics and Heat Transfer [Текст] : Engineering Research / J.G. Knudsen, D.L. Katz. — Michigan : Engineering Research Institute, 1953. — 243 p.
- General Method and Thermodynamic Tables for Computation of Equlibrium Composition and Temperature of Chemical Reactions [Текст] : Report / National Advisory Committee For Aeronautics. — Washington : U.S. Government Printing Office, 1951. — 57 p.
- General Method of Thermodynamics Tables for Computation of Equilibrium Composition and Temperature of Chemical Reactions [Текст] : Report / National Advisory Committee for Aeronautics. — Washington : U.S. Gowernment Printing Office, 1951. — 57 p.
- Graphical Presentation of Difference Solutions for Transient Radial Heat Conduction in Hollow Cylinders With Heat Transfer at the Inner Radius and Finite Slabs with Heat Transfer at one Boundary [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1960. — 49 p.
- Hot-wire Calorimetry: Theory and Application to Lon Rocket Research [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1961. — 45 p.
- 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.
- Loads and Deformations of Buckled Rectangular Plates [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1959. — 27 p.
- Local Heat Transfer and Recovery Temperatures on a Yawed Cylinder at a Mach Number of 4.15 and High Reynolds Numbers [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1961. — 25 p.
- Local Instability of the Elements of a Truss-Core Sandwich Plate [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1959. — 13 p.
- Mass Transfer Cooling Near the Stagnation Point [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1959. — 16 p.
- Method for Calculation of Laminar Heat Transfer in Air Flow Around Cylinders of Arbitrary Cross Section ( Including Large Temperature Differences and Transpiration Cooling ) [Текст] : Report / National Advisory Committee For Aeronautics. — Washington : U.S. Government Printing Office, 1953. — 29 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.
- Normal Component of Inducted Velocity for Entire Field of a Uniformly Loaded Lifting Rotor With Highly Swept Wake as Determined by Electromagnetic Analog [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1959. — 23 p.
- Numerical Analysis of Heat Flow [Текст] / G.M. Dusinberre. — New York : McGraw-Hill Book Company, Inc., 1949. — 227 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 Fully Developed Channel Flows: Some Solutions and Limitations, and Effects of Compressibility, Variable Properties, and Body Forces [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1959. — 22 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.
- Review of Experimental Investigation of Liquid-Metal Heat Transfer [Текст] : Report / NACA. — Washington : U.S. Government Printing Office, 1956. — 33 p.
- Similar Solutions for the Compressible Laminar Boundry Layer With Heat Transfer and Pressure Gradient [Текст] : Report / NACA. — Washington : U.S. Government Printing Office, 1956. — 38 p.
- Some Possibilities of Using Gas Mixtures Other Than Air in Aerodynamic Research [Текст] : Report / NACA. — Washington : U.S. Government Printing Office, 1956. — 22 p.
- Stability of a Horizontal Fluid Layer With Unsteady Heating From Below and Time-Dependent Body Force [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1959. — 15 p.
- Stagnation-Point Shiekding by Melting and Vaporization [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1959. — 24 p.
- Survey of Hydrogen Combution Properties [Текст] : Report / NACA. — Washington : U.S. Government Printing Office, 1958. — 34 p.
- Theoretical and Experimental Investigation of Heat Conduction in Air, Including Effects of Oxygen Dissociation [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1959. — 25 p.
- Theoretical and Experimental Investigation of Heat Transfer by Laminar Natural Convection Between Parallel Plates [Текст] : Report / National Advisory Committee for Aeronautics. — Washington : U.S. Government Printing Office, 1955. — 7 p.
- Theory and Apparatus for Measurement of Emissivity for Radiative Cooling of Hypersonic Aircraft With Data for Inconel, Inconel X, Stainless Steel 303, and Titanium Alloy RS-120 [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1961. — 24 p.
- The Propagation of Plane Acoustic Waves in a Radiating Gas [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1962. — 54 p.
- Thermodynamics of Fluid Flow [Текст] / N.A. Hall. — London : Logmans, Green and Co, 1957. — 278 p.
- The Similarity Rules for Second-Order Subsonic and Supersonic Flow [Текст] : Report / NACA. — Washington : U.S. Government Printing Office, 1958. — 8 p.
- XIII International Symposium on Rarefied Gas Dynamics, Novosibirsk, July 5-9, 1982 [Текст] = 13 Международный симпозиум по динамике разреженных газов : Book of Abstracts / International Symposium on Rarefied Gas Dynamics , Novosibirsk. — Novosibirsk : Institute of Thermophysics, 1982. — 291 p.
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