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Volumn 115, Issue 3, 1998, Pages 299-312

Structure and acoustic-pressure response of hydrogen-oxygen diffusion flames at high pressure

Author keywords

[No Author keywords available]

Indexed keywords

ASYMPTOTIC ANALYSIS; BOOSTERS (ROCKET); ENGINES; HYDROGEN; OXYGEN; ROCKET ENGINES; ROCKETS; SENSITIVITY ANALYSIS;

EID: 0031814311     PISSN: 00102180     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0010-2180(98)00007-8     Document Type: Article
Times cited : (40)

References (24)
  • 2
    • 0003319057 scopus 로고
    • Liquid Propellant Rocket Combustion Instability
    • AIAA, Washington, DC
    • Yang, V., and Anderson, W. E., Eds., Liquid Propellant Rocket Combustion Instability, Vol. 169, Progress in Astronautics and Aeronautics, AIAA, Washington, DC, 1995.
    • (1995) Progress in Astronautics and Aeronautics , vol.169
    • Yang, V.1    Anderson, W.E.2
  • 14
    • 0020904112 scopus 로고
    • A Fortran Computer Code Package for the Evaluation of Gas-Phase Viscosities, Conductivities, and Diffusion Coefficients
    • Kee, R. J., Warnatz, J., and Miller, J. A. (1983). A Fortran Computer Code Package for the Evaluation of Gas-Phase Viscosities, Conductivities, and Diffusion Coefficients. Sandia National Laboratories Report No. SAND83-8209.
    • (1983) Sandia National Laboratories Report No. SAND83-8209
    • Kee, R.J.1    Warnatz, J.2    Miller, J.A.3
  • 23


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.