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Volumn 13, Issue 4, 1997, Pages 543-551

Mach 6 testing of a scramjet engine model

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTION; FOURIER TRANSFORMS; FUEL INJECTION; HEAT FLUX; HYDROGEN; INTAKE SYSTEMS; PRESSURE MEASUREMENT; TEMPERATURE MEASUREMENT;

EID: 0031186781     PISSN: 07484658     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.5201     Document Type: Article
Times cited : (90)

References (21)
  • 3
    • 33645791753 scopus 로고    scopus 로고
    • Calibration Studies of Nozzle Flow in Ramjet Engine Test Facility
    • Committee of International Symposium on Space Technology and Science, Paper 96-d-14, Gifu, Japan, May
    • Hiraiwa, T., Mitani, T., Izumikawa, M., and Ono, F., "Calibration Studies of Nozzle Flow in Ramjet Engine Test Facility," The 20th International Symposium on Space Technology and Science, Committee of International Symposium on Space Technology and Science, Paper 96-d-14, Gifu, Japan, May 1996.
    • (1996) The 20th International Symposium on Space Technology and Science
    • Hiraiwa, T.1    Mitani, T.2    Izumikawa, M.3    Ono, F.4
  • 7
    • 0004108629 scopus 로고
    • McGraw - Hill, New York
    • White, F. M., Viscous Fluid Flow, McGraw - Hill, New York, 1974, pp. 632-640.
    • (1974) Viscous Fluid Flow , pp. 632-640
    • White, F.M.1
  • 8
    • 0029196878 scopus 로고
    • Review and Development of Base Pressure and Base Heating Correlations in Supersonic Flow
    • Lamb, J. P., and Oberkampf, W. L., "Review and Development of Base Pressure and Base Heating Correlations in Supersonic Flow," Journal of Spacecraft and Rockets, Vol. 32, No. 1, 1995, pp. 8-23.
    • (1995) Journal of Spacecraft and Rockets , vol.32 , Issue.1 , pp. 8-23
    • Lamb, J.P.1    Oberkampf, W.L.2
  • 9
    • 0015768905 scopus 로고
    • An Approximate Approach to Base Flow behind Two-Dimensional Rearward-Facing Steps Placed in a Uniform Supersonic Stream
    • Tokyo, Japan, Nov.
    • Karashima, K., and Hasegawa, K., "An Approximate Approach to Base Flow Behind Two-Dimensional Rearward-Facing Steps Placed in a Uniform Supersonic Stream," Inst. of Space and Aeronautical Science, Rept. 501, Tokyo, Japan, Nov. 1973.
    • (1973) Inst. of Space and Aeronautical Science, Rept. 501
    • Karashima, K.1    Hasegawa, K.2
  • 12
    • 84997080025 scopus 로고
    • Effect of Scale on Supersonic Combustor Performance
    • June
    • Diskin, G. S., and Northam, G. B., "Effect of Scale on Supersonic Combustor Performance," AIAA Paper 87-2164, June 1987.
    • (1987) AIAA Paper 87-2164
    • Diskin, G.S.1    Northam, G.B.2
  • 15
    • 0015078989 scopus 로고
    • A Unified Analysis of Gaseous Jet Penetration
    • Billig, F. S., Orth, R. C., and Lasky, M., "A Unified Analysis of Gaseous Jet Penetration," AIAA Journal, Vol. 9, No. 6, 1971, pp. 1048-1057.
    • (1971) AIAA Journal , vol.9 , Issue.6 , pp. 1048-1057
    • Billig, F.S.1    Orth, R.C.2    Lasky, M.3
  • 16
    • 85003264321 scopus 로고
    • Shock-Wave Shapes Around Spherical- and Cylindrical-Nosed Bodies
    • Billig, F. S., "Shock-Wave Shapes Around Spherical- and Cylindrical-Nosed Bodies," Journal of Spacecraft and Rockets, Vol. 4, No. 6, 1967, pp. 822, 823.
    • (1967) Journal of Spacecraft and Rockets , vol.4 , Issue.6 , pp. 822
    • Billig, F.S.1
  • 19
    • 0015667888 scopus 로고
    • Prediction of Precombustion Shock Wall Pressure Distributions in Scramjet Engines
    • Waltrup, P. J., and Billig, F. S., "Prediction of Precombustion Shock Wall Pressure Distributions in Scramjet Engines," Journal of Spacecraft and Rockets, Vol. 10, No. 9, 1973, pp. 620-622.
    • (1973) Journal of Spacecraft and Rockets , vol.10 , Issue.9 , pp. 620-622
    • Waltrup, P.J.1    Billig, F.S.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.