Possibilities of using supersonic combustion for air vehicles in mid-hypersonic range are examined by considering its propulsion aspect and conditions of suitable supersonic combustion; study of combustion in supersonic stream shows evolution of ratio of heat inputs to stagnation enthalpy of air as function of flight Mach number; it is possible to obtain without any auxiliary device stable combustion in supersonic flow when air temperature is high enough for autoignition of air-fuel mixture; regions for which it is possible to assure combustion by autoignition without being limited by heat input considerations are determined.
Application of supersonic combustion to ramjets
Aircraft Eng
Aircraft Engineering ; 38 , n 2
1966
3 pages
Aufsatz (Zeitschrift)
Englisch
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The potential of supersonic combustion ramjets
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|The Potential of Supersonic Combustion Ramjets
British Library Conference Proceedings | 1995
|Application of Supersonic Combustion to Ramjets
Emerald Group Publishing | 1966
|