Description of scramjet and analysis of its performance in high hypersonic speed range in excess of Mach 10; effect of inlet operation on overall performance is considered; cycle performance of scramjets at given flight condition depends on mode of heat addition, fuel type, injection conditions, equivalence ratio, combustion efficiency, nozzle efficiency including nonequilibrium effects, and overall engine area ratio; problem areas comprise inviscid hypersonic flow field, three-dimensional boundary layers, mixing, combustion kinetics, and nozzle flow.
Really high speed propulsion by scramjets
Aircraft Eng
Aircraft Engineering ; 38 , n 1
1966
6 pages
Aufsatz (Zeitschrift)
Englisch
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