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Volumn 18, Issue 4, 2002, Pages 943-952

Characterization of expansion tube flows for hypervelocity combustion studies

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; COMBUSTION; COMPOSITION; ENTHALPY; FLIGHT SIMULATORS; FUEL INJECTION; GAS FUELS; JETS; STEADY FLOW;

EID: 0036638671     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/2.6021     Document Type: Article
Times cited : (27)

References (29)
  • 8
    • 84963839269 scopus 로고
    • Recent experiments on hypersonic combustion in an expansion tube test facility
    • edited by J. D. Buckmaster, T. L. Jackson, and A. Kumar, Kluwer Academic Publisher
    • (1994) Combustion in High-Speed Flows , pp. 53-91
    • Erdos, J.I.1
  • 10
    • 21344448572 scopus 로고    scopus 로고
    • Transverse and parallel injection of hydrogen with supersonic combustion in a shock tunnel
    • Springer-Verlag, Berlin
    • (1996) Shock Waves , vol.6 , pp. 53-59
    • Wendt, M.N.1    Stalker, R.J.2
  • 16
    • 85086056271 scopus 로고    scopus 로고
    • Bridge from hypersonic aeropropulsion ground test data to flight performance
    • June
    • (1998) AIAA Paper , vol.98 , Issue.2494
    • Erdos, J.I.1
  • 24
    • 0001678156 scopus 로고
    • Flow nonuniformity in shock tubes operating at maximum test times
    • (1966) Physics of Fluids , vol.9 , Issue.10 , pp. 1907-1912
    • Mirels, H.1
  • 29


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.