Scramjet Propulsion

Author:

Murthy S.N.B.,Curran E.T.

Publisher

American Institute of Aeronautics and Astronautics

Reference66 articles.

1. Anderson,G.Y.,and Clayton-Rogers,R."AComparisonofExperimentalSupersonic Combustor Performance with an Empirical Correlation on Non-Reactive MixingResults,"NASATMX-2429,1971.

2. Anderson, M.,and Ortwerth,P."Three Dimensional Hypersonic Inlets - Low Speed Performance,"AIAAPaper 91-5021,1991.

3. Auslender,A.H."AnApplicationofDistortionAnalysistoScramjet-Combustor Performance Assessment,"JANNAFWorkshop on Scramjet Combustor PerformanceFinal Report,1996.

4. Baker,N.R.,Northam, G.B.,Stouffer, S.D., and Capriotti,D.P."Evaluation of Scramjet Nozzle Configurations and Film Coolingfor Reduction of WallHeating," AIAAPaper 93-0744,1993.

5. Baev,V.K.,Golovchev,V.I.,Tret'yakov,P.K.,Garanin,A.F,Konstantinovskiy,V. A.,andYasakov,V.A."Combustion inSupersonicFlow,"NASATM-77822,1986.

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