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Volumn 17, Issue 3, 1998, Pages 217-229

Evaluation of the performance of supersonic exhaust diffuser using scaled down models

Author keywords

[No Author keywords available]

Indexed keywords

EXHAUST SYSTEMS (ENGINE); NOZZLES; ROCKET ENGINES; SPECIFIC HEAT OF GASES; SUPERSONIC FLOW; VACUUM APPLICATIONS;

EID: 0032123465     PISSN: 08941777     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0894-1777(98)00002-8     Document Type: Article
Times cited : (58)

References (13)
  • 1
    • 0010676389 scopus 로고
    • High altitude and space simulation testing
    • B.H. Goethert, High altitude and space simulation testing, ARS Journal (1962) 872-882.
    • (1962) ARS Journal , pp. 872-882
    • Goethert, B.H.1
  • 6
    • 0015677401 scopus 로고
    • Structure of shock waves in cylindrical ducts
    • Waltrup P.J., Billig F.S. Structure of shock waves in cylindrical ducts. AIAA Journal. 11(10):1973;1404-1408.
    • (1973) AIAA Journal , vol.11 , Issue.10 , pp. 1404-1408
    • Waltrup, P.J.1    Billig, F.S.2
  • 13
    • 0023844053 scopus 로고
    • Describing the uncertainties in experimental results
    • R.J. Moffat, Describing the uncertainties in experimental results, Experimental Thermal and Fluid Science, vol. I, (1988) pp 3-17.
    • (1988) Experimental Thermal and Fluid Science , vol.1 , pp. 3-17
    • Moffat, R.J.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.