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Volumn , Issue , 1995, Pages

A pulse detonation engine performance model

Author keywords

[No Author keywords available]

Indexed keywords

JET ENGINES; PROPULSION;

EID: 84964413548     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (32)

References (20)
  • 4
    • 0000890978 scopus 로고
    • Intermittent Detonation as a Thrust-Prcdncing Mechanism
    • May
    • Nicholls, J.A., Wilkinson, H.R., and Morrison, R.B., “Intermittent Detonation as a Thrust-Prcdncing Mechanism” Jet Propulsion, Val. 27, May, 1957.
    • (1957) Jet Propulsion , vol.27
    • Nicholls, J.A.1    Wilkinson, H.R.2    Morrison, R.B.3
  • 5
    • 84964555314 scopus 로고
    • Shock Tube Experiments for the Development of a Hydrogen-Fueled Pulse Detonation Engine
    • AIAA 95-2578, San Diego, CA, July 10-12
    • Hinkey, J.B., Bussing, T.R.A., and Kaye, L., “Shock Tube Experiments for the Development of a Hydrogen-Fueled Pulse Detonation Engine” AIAA 95-2578, 31st AIAA/ASME/SAE/ASEE Joint PropnIsion Conference, San Diego, CA, July 10-12, 1995.
    • (1995) 31St AIAA/ASME/SAE/ASEE Joint Propnision Conference
    • Hinkey, J.B.1    Bussing, T.R.A.2    Kaye, L.3
  • 8
    • 0004175904 scopus 로고
    • Preliminary Numerical Simulations of a Pulsed Detonation Wave Engine
    • AIAA Paper 88-2960, Boston, MA, July 11-13
    • Cambier, J. L. and Adelman, H.G., “Preliminary Numerical Simulations of a Pulsed Detonation Wave Engine,” AIAA Paper 88-2960, 24th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Boston, MA, July 11-13, 1988.
    • (1988) 24Th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
    • Cambier, J.L.1    Adelman, H.G.2
  • 10
    • 85003666489 scopus 로고
    • Compntational Analysis of Pulsed Detonation Engines and Applications
    • AIAA Paper 90-0460, January 8-11
    • Eidelman, S., Grossmann, W., and Lottati, I., “Compntational Analysis of Pulsed Detonation Engines and Applications,” AIAA Paper 90-0460, 28th AIM Aerospace Sciences Meeting, Reno NV, January 8-11, 1990.
    • (1990) 28Th AIM Aerospace Sciences Meeting, Reno NV
    • Eidelman, S.1    Grossmann, W.2    Lottati, I.3
  • 12
    • 0003492511 scopus 로고
    • Computational Fluid Dynamic Analysis of the Pulse Detonation Engine Concept
    • AIAA 94-0264, Reno NV, January 10-13
    • Lynch, E.D., Edelman, R., and Palaniswamy, S., “Computational Fluid Dynamic Analysis of the Pulse Detonation Engine Concept,” AIAA 94-0264, 32nd AIAA Aerospace Sciences Meeting & Exhibit, Reno NV, January 10-13, 1994.
    • (1994) 32Nd AIAA Aerospace Sciences Meeting & Exhibit
    • Lynch, E.D.1    Edelman, R.2    Palaniswamy, S.3
  • 13
    • 0012150806 scopus 로고
    • A Rotary Valve Multiple Combustor Pulse Detonation Engine (RVMPDE
    • AUA 95-2571, San Diego, CA, July 10-12
    • Bussing, T. R. A., “A Rotary Valve Multiple Combustor Pulse Detonation Engine (RVMPDE)”, AUA 95-2571, 31st AIAA/ASME/SAE/ASEE Joint Propulsion Conference, San Diego, CA, July 10-12, 1995.
    • (1995) 31St AIAA/ASME/SAE/ASEE Joint Propulsion Conference
    • Bussing, T.R.A.1
  • 15
    • 84964553271 scopus 로고
    • Experimental Characterization of the Detonation Properties of Hydrocarbon Fuels for the Development of a Pulse Detonation Engine
    • AIAA Paper 95-3154, San Diego, CA, July 10-12
    • Ting, J. M., Bussing, T. R. A., and Hinkey, J. B., “Experimental Characterization of the Detonation Properties of Hydrocarbon Fuels for the Development of a Pulse Detonation Engine,“AIAA Paper 95-3154, 31st AIAAIASMEISAEIASEE Joint Propulsion Conference, San Diego, CA, July 10-12.1995.
    • (1995) 31St AIAAIASMEISAEIASEE Joint Propulsion Conference
    • Ting, J.M.1    Bussing, T.R.A.2    Hinkey, J.B.3
  • 20
    • 84964508255 scopus 로고
    • AS1 Consulting Report, April 4, 1994
    • Lidstone, G., “Nozzle Performance,” AS1 Consulting Report, April 4, 1994.1994
    • (1994) Nozzle Performance
    • Lidstone, G.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.