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Volumn 342, Issue , 1997, Pages 1-35

The interaction of a shock wave with a laminar boundary layer at a compression corner in high-enthalpy flows including real gas effects

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; ENTHALPY; FLOW INTERACTIONS; FLOW VISUALIZATION; GAS DYNAMICS; HEAT TRANSFER; LAMINAR FLOW; SHOCK WAVES;

EID: 0031177720     PISSN: 00221120     EISSN: None     Source Type: Journal    
DOI: 10.1017/S0022112097005673     Document Type: Article
Times cited : (61)

References (102)
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    • BALL, K. O. W. 1971 AIAA J. 9, 2080-2081.
    • (1971) AIAA J. , vol.9 , pp. 2080-2081
    • Ball, K.O.W.1
  • 18
    • 0007695586 scopus 로고
    • CURLE, L. 1961 Aero. Q. 12, 309-336.
    • (1961) Aero. Q. , vol.12 , pp. 309-336
    • Curle, L.1
  • 40
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  • 50
    • 0000483682 scopus 로고
    • HOLDEN, M. S. 1971b AIAA J. 9, 2296-2298.
    • (1971) AIAA J. , vol.9 , pp. 2296-2298
    • Holden, M.S.1
  • 55
    • 0017559278 scopus 로고
    • IKAWA, H. 1977 AIAA J. 14, 669-675.
    • (1977) AIAA J. , vol.14 , pp. 669-675
    • Ikawa, H.1
  • 77
  • 93
    • 0024882946 scopus 로고
    • STALKER, R. J. 1989b AIAA J. 27, 1761-1769.
    • (1989) AIAA J. , vol.27 , pp. 1761-1769
    • Stalker, R.J.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.