The aerodynamical analysis of body in hypersonic source flow field
Abstract
The hypersonic source flow field, a typical non-uniform free stream flow field, around a body was investigated. Various aerodynamic coefficients were obtained by means of Newton's theory. Analysis of the effects of the non-uniformity of the free stream was emphasized. It was found that under the condition of small angle of attack the analytical results are satisfactory.
- Publication:
-
Acta Mechanica
- Pub Date:
- November 1981
- Bibcode:
- 1981AcMec.......60L
- Keywords:
-
- Aerodynamic Coefficients;
- Flow Distribution;
- Free Flow;
- Hypersonic Flow;
- Shock Tunnels;
- Aerodynamic Configurations;
- Angle Of Attack;
- Cartesian Coordinates;
- Conical Bodies;
- Newton Theory;
- Pitching Moments;
- Pressure Measurement;
- Slender Bodies;
- Spherical Shells;
- Fluid Mechanics and Heat Transfer