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Volumn 12, Issue 2, 1996, Pages 431-433

Mixing pressure-rise parameter for effect of nozzle geometry in diffuser-ejectors

Author keywords

[No Author keywords available]

Indexed keywords

DIFFUSERS (FLUID); MATHEMATICAL MODELS; MIXING; NOZZLES; PRESSURE EFFECTS; SPACECRAFT PROPULSION;

EID: 0030106345     PISSN: 07484658     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.24049     Document Type: Article
Times cited : (11)

References (10)
  • 1
    • 0010676389 scopus 로고
    • High Altitude and Space Simulation Testing
    • June
    • Goethert, B. H., "High Altitude and Space Simulation Testing," ARS Journal, Vol. 32, June 1962, pp. 872-882.
    • (1962) ARS Journal , vol.32 , pp. 872-882
    • Goethert, B.H.1
  • 7
    • 85003260888 scopus 로고
    • Methods for Determining the Performance of Ejector-Diffuser Systems
    • German, R. C., Bauer, R. C., and Panesci, J. H., "Methods for Determining the Performance of Ejector-Diffuser Systems," Journal of Spacecraft and Rockets, Vol. 3, No. 2, 1966, pp. 193-200.
    • (1966) Journal of Spacecraft and Rockets , vol.3 , Issue.2 , pp. 193-200
    • German, R.C.1    Bauer, R.C.2    Panesci, J.H.3
  • 8
    • 0028261987 scopus 로고
    • Supersonic Flow in the Second Throat Ejector-Diffuser System
    • Chen, F., Liu, C. F., and Yang, J. Y., "Supersonic Flow in the Second Throat Ejector-Diffuser System," Journal of Spacecraft and Rockets, Vol. 31, No. 1, 1994, pp. 123-129.
    • (1994) Journal of Spacecraft and Rockets , vol.31 , Issue.1 , pp. 123-129
    • Chen, F.1    Liu, C.F.2    Yang, J.Y.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.