Hypersonic flow of viscous radiating gas around a cone
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Abstract
When a body moves in a gas at high supersonic speed, the gas located in the area between the surface of the body and the shock wave heats up to a temperature of several thousand degrees. At such a temperature, the flow parameters can be significantly affected by the heat exchange of radiation between the gas particles, as well as between the gas and the surface of the streamlined body. The heat emission of the gas in the shock layer leads to a decrease in its temperature and an increase in density.
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References
- Cherny G. G. Gas flows at high supersonic speed. Fizmatgiz, 1959.
- Lyubimov G. A. The flow of bodies around a stream of imperfect gas at high supersonic speeds. Proc. AS USSR, OTN., Mechanics and Mechanical Engineering, 1959, No. 1.
- Hayes, W. D., Probstin, R. F. Theory of hypersonic flows. FL, 1962.
- Kolton G. A. The flow of radiating gas in the vicinity of the critical point of a blunt-nosed body. Bulletin of LSU, 1964, No. 13.
- Kolton G. A. The flow around a cone by a hypersonic flow of an inviscid radiating gas. Bulletin of LSU, 1965, No. 7.
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