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Volumn 15, Issue 3, 1999, Pages 401-407

Performance evaluation of scramjet combustors using kinetic energy and combustion efficiencies

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTION; DUCTS; FUEL INJECTION; HEAT LOSSES; JET ENGINES; KINETIC ENERGY; NOZZLES; PERFORMANCE;

EID: 0033132836     PISSN: 07484658     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.5458     Document Type: Article
Times cited : (11)

References (19)
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    • Contensou, P., Marguet, R., and Huet, C., "Etude Théorique et Expérimentale d'un Statoréacteur a Combustion Mixte (Domaine de vol Mach 3,5/7)," La Recherche Aérospatiale, No. 1973-5, 1973, pp. 259-274.
    • (1973) La Recherche Aérospatiale , pp. 259-274
    • Contensou, P.1    Marguet, R.2    Huet, C.3
  • 7
    • 0344063994 scopus 로고
    • Combustor kinetic energy efficiency analysis of the hypersonic research engine data
    • June
    • Hoose, K. V., "Combustor Kinetic Energy Efficiency Analysis of the Hypersonic Research Engine Data," AIAA Paper 94-2818, June 1994.
    • (1994) AIAA Paper 94-2818
    • Hoose, K.V.1
  • 8
    • 0345357597 scopus 로고
    • Energy analysis of high speed vehicle systems
    • Jan.
    • Murthy, S. N. B., and Czysz, P., "Energy Analysis of High Speed Vehicle Systems," AIAA Paper 90-0089, Jan. 1990.
    • (1990) AIAA Paper 90-0089
    • Murthy, S.N.B.1    Czysz, P.2
  • 9
    • 85003322424 scopus 로고
    • Investigation of scramjet injection strategies for high mach number flows
    • Riggins, D. W., McClinton, C. R., Rogers, R. C., and Bittner, R. D., "Investigation of Scramjet Injection Strategies for High Mach Number Flows," Journal of Propulsion and Power, Vol. 11, No. 3, 1995, pp. 409-418.
    • (1995) Journal of Propulsion and Power , vol.11 , Issue.3 , pp. 409-418
    • Riggins, D.W.1    McClinton, C.R.2    Rogers, R.C.3    Bittner, R.D.4
  • 10
    • 0031099209 scopus 로고    scopus 로고
    • Thrust loss in hypersonic engines part 1: Methodology
    • Riggins, D. W., McClinton, C. R., and Vitt, P. H., "Thrust Loss in Hypersonic Engines Part 1: Methodology," Journal of Propulsion and Power, Vol. 13, No. 2, 1997, pp. 281-287.
    • (1997) Journal of Propulsion and Power , vol.13 , Issue.2 , pp. 281-287
    • Riggins, D.W.1    McClinton, C.R.2    Vitt, P.H.3
  • 11
    • 0031097942 scopus 로고    scopus 로고
    • Evaluation of performance loss methods for high-speed engines and engine components
    • Riggins, D. W., "Evaluation of Performance Loss Methods for High-Speed Engines and Engine Components," Journal of Propulsion and Power, Vol. 13, No. 2, 1997, pp. 296-304.
    • (1997) Journal of Propulsion and Power , vol.13 , Issue.2 , pp. 296-304
    • Riggins, D.W.1
  • 16
    • 0031235816 scopus 로고    scopus 로고
    • Comparison of Scramjet engine performance in Mach 6 vitiated and storage heated air
    • Mitani, T., Hiraiwa, T., Sato, S., Tomioka, S., Kanda, T., and Tani, T., "Comparison of Scramjet Engine Performance in Mach 6 Vitiated and Storage Heated Air," Journal of Propulsion and Power, Vol. 13, No. 5, 1997, pp. 635-642.
    • (1997) Journal of Propulsion and Power , vol.13 , Issue.5 , pp. 635-642
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  • 17
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    • Experiment on reaction quenching in gas sampling probes for Scramjet engine testing
    • The Combustion Inst., Pittsburgh, PA
    • Mitani, T., Chinzei, N., and Masuya, G., "Experiment on Reaction Quenching in Gas Sampling Probes for Scramjet Engine Testing," 27th Symposium (International) on Combustion, The Combustion Inst., Pittsburgh, PA, 1998, pp. 2151-2156.
    • (1998) 27th Symposium (International) on Combustion , pp. 2151-2156
    • Mitani, T.1    Chinzei, N.2    Masuya, G.3
  • 19
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.