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Volumn , Issue , 1999, Pages

Conventional/laser diagnostics to assess flow quality in a combustion-heated facility

Author keywords

[No Author keywords available]

Indexed keywords

COHERENT SCATTERING; COMBUSTION; COMBUSTION CHAMBERS; COMPUTATIONAL FLUID DYNAMICS; FLOW FIELDS; NASA; PROPULSION; RAMAN SCATTERING; RAMAN SPECTROSCOPY; ROCKET NOZZLES; VISUALIZATION;

EID: 84963877991     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (4)

References (10)
  • 2
    • 3242873769 scopus 로고    scopus 로고
    • Specification of Model Entrance Conditions for Scramjet Testing in Vitiated Air
    • Cutler, A. D., “Specification of Model Entrance Conditions for Scramjet Testing in Vitiated Air,” AIAA Journal, 36(7), 1200-1207 (1998).
    • (1998) AIAA Journal , vol.36 , Issue.7 , pp. 1200-1207
    • Cutler, A.D.1
  • 10
    • 0027553769 scopus 로고
    • Coher-ent Anti-Stokes Raman Spectroscopy Temperature Measurements in a Hydrogen-Fueled Supersonic Combustor
    • Smith, M. W., Jarrett, O. Jr., Antcliff, R. R., Northam, G. B., Cutler, A. D., and Taylor, D. J., “Coher-ent Anti-Stokes Raman Spectroscopy Temperature Measurements in a Hydrogen-Fueled Supersonic Combustor,” Journal of Propulsion and Power, 9(2), 163-168 (1993).
    • (1993) Journal of Propulsion and Power , vol.9 , Issue.2 , pp. 163-168
    • Smith, M.W.1    Jarrett, O.2    Antcliff, R.R.3    Northam, G.B.4    Cutler, A.D.5    Taylor, D.J.6


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.