Hypersonic flow of viscous radiating gas around a cone
Authors:
Abstract
During the motion of a body in a gas at a high supersonic speed, the gas located in the region between the surface of the body and the shock wave is heated to a temperature of several thousand degrees. At such a temperature, the flow parameters can be significantly affected by radiative heat exchange between the gas particles, as well as between the gas and the surface of the body in the flow. The radiative emission of the gas in the shock layer leads to a decrease in its temperature and an increase in density.
Область исследования:
(Archived) Without section
Funding:
None
References
- Cherny G. G. Gas Flows at High Supersonic Speed. Fizmatgiz, 1959 (in Russian)
- Lyubimov G. A. Flow past bodies by a stream of non-ideal gas at high supersonic speeds. Izv. AN SSSR, OTN, Mekhanika i mashinostroenie , , 1959, No. 1 (in Russian)
- Hayes W. D., Probstein R. F. Theory of Hypersonic Flows. IL, 1962 (in Russian)
- Kolton G. A. Flow of a radiating gas in the vicinity of the stagnation point of a blunt-nosed body. Vestnik LGU , 1964, No. 13 (in Russian)
- Kolton G. A. Flow past a cone by a hypersonic stream of inviscid radiating gas. Vestnik LGU , 1965, No. 7 (in Russian)