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Volumn , Issue , 1996, Pages

Preliminary surface pressure measurements of transitional, hypersonic shock boundary layer interactions

Author keywords

[No Author keywords available]

Indexed keywords

HYPERSONIC BOUNDARY LAYERS; PRESSURE MEASUREMENT; REYNOLDS NUMBER; SPACECRAFT;

EID: 84983155111     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (6)

References (17)
  • 3
    • 0028378940 scopus 로고
    • Experimental, Analytical, and Computational Methods Applied to Hypersonic Compression Ramp Flows
    • Simeonides, G., Haase, W. and Manna, M., “Experimental, Analytical, and Computational Methods Applied to Hypersonic Compression Ramp Flows,” AIAA Journal, Vol. 32, No. 2, 1994, pp. 301-310.
    • (1994) AIAA Journal , vol.32 , Issue.2 , pp. 301-310
    • Simeonides, G.1    Haase, W.2    Manna, M.3
  • 4
    • 0029193848 scopus 로고
    • Viscous Interaction Phenomena in Hypersonic Wedge Flow
    • de Luca, L., Cardone, G., Aymer de laChevalerie, D. and Fonteneau, A., ‘Viscous Interaction Phenomena in Hypersonic Wedge Flow,” AIAA Journal, Vol. 33, No. 12, 1995, pp. 2293-2298.
    • (1995) AIAA Journal , vol.33 , Issue.12 , pp. 2293-2298
    • De Luca, L.1    Cardone, G.2    Aymer Delachevalerie, D.3    Fonteneau, A.4
  • 7
    • 84983209755 scopus 로고
    • Investigation of Separated Flow in Supersonic and Subsonic Streams with Emphasis on the Effects of Transition,” NACA Report No. 1356
    • Chapman, D. R., Kuehn, D. M. and Larson, H. K., “Investigation of Separated Flow in Supersonic and Subsonic Streams with Emphasis on the Effects of Transition,” NACA Report No. 1356, 1958.
    • (1958)
    • Chapman, D.R.1    Kuehn, D.M.2    Larson, H.K.3
  • 10
    • 85003369949 scopus 로고
    • Hypersonic Turbulent Expansion-Corner Flow with Shock Impingement
    • Chung, K.-M. and Lu, F. K., “Hypersonic Turbulent Expansion-Corner Flow with Shock Impingement,” Journal of Propulsion, Vol. 11, No. 3, 1995, pp. 441-447.
    • (1995) Journal of Propulsion , vol.11 , Issue.3 , pp. 441-447
    • Chung, K.-M.1    Lu, F.K.2
  • 12
    • 84983098848 scopus 로고    scopus 로고
    • Report WL-TR-94-3012, Wright Laboratory, Wright- Patterson Air Force Base, Ohio; also, Transitional and Turbulent Compressible Flows, 'FED, ASME
    • Kimmel, R. L., “The Effect of Pressure Gradient on Transition Zone Length in Hypersonic Boundary Layers,” Report WL-TR-94-3012, Wright Laboratory, Wright- Patterson Air Force Base, Ohio; also, Transitional and Turbulent Compressible Flows, 'FED Vol. 151, ASME, pp. 117-127.
    • The Effect of Pressure Gradient on Transition Zone Length in Hypersonic Boundary Layers , vol.151 , pp. 117-127
    • Kimmel, R.L.1
  • 13
    • 0017493293 scopus 로고
    • Similitude Properties of High-speed Laminar and Turbulent Boundary-Layer Incipient Separation
    • Inger, G. R., “Similitude Properties of High-speed Laminar and Turbulent Boundary-Layer Incipient Separation,” AIAA Journal, Vol. 15, No. 5, 1977, pp. 619-623.
    • (1977) AIAA Journal , vol.15 , Issue.5 , pp. 619-623
    • Inger, G.R.1
  • 14
    • 0014971375 scopus 로고
    • Boundary-Layer Displacement and Leading-Edge Bluntness Effects on Attached and Separated Laminar Boundary Layers in a Compression Corner. Part II: Experimental Study
    • Holden, M. S., “Boundary-Layer Displacement and Leading-Edge Bluntness Effects on Attached and Separated Laminar Boundary Layers in a Compression Corner. Part II: Experimental Study,” AIAA Journal, Vol. 9, No. 1, 1971, pp. 84-93.
    • (1971) AIAA Journal , vol.9 , Issue.1 , pp. 84-93
    • Holden, M.S.1
  • 15
    • 0016046540 scopus 로고
    • The Hypersonic Laminar Boundary Layer near Sharp Compression and Expansion Corners
    • Bloy, A. W. and Georgeff, M. P., “The Hypersonic Laminar Boundary Layer near Sharp Compression and Expansion Corners,” Joui-nal of Fluid Mechanics, Vol. 63, 1974, pp. 431-447.
    • (1974) Joui-Nal of Fluid Mechanics , vol.63 , pp. 431-447
    • Bloy, A.W.1    Georgeff, M.P.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.