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Volumn 23, Issue 3, 2007, Pages 566-574

Experimental investigations of the performance and unsteady behavior of a supersonic intake

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; GEOMETRY; RAMJET ENGINES; SUPERSONIC FLOW; TEMPERATURE MEASUREMENT; WIND TUNNELS;

EID: 34250363185     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/1.25103     Document Type: Article
Times cited : (35)

References (19)
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  • 4
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  • 6
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    • Characteristics of Multiple Shock Wave/Turbulent Boundary Layer Interaction in Rectangular Ducts
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    • (1989)
    • Carrol, B.F.1    Dutton, J.C.2
  • 8
    • 0008150575 scopus 로고
    • Practical Intake Aerodynamic Design
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    • (1993) AIAA Education Series
    • Seddon, J.1    Goldsmith, E.L.2
  • 9
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    • Inlet and Propulsion Integration of RAM Propelled Vehicles," AGARD FDP Special Course on "Aerothermodynamics and Propulsion Integration for Hypersonic Vehicles
    • April
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    • (1996) NATO
    • Bissinger, N.C.1
  • 10
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    • Three- Dimensional Show-Wave/Boundary-Layer Interactions with Bleed
    • Oct
    • Shih, T. I.-P., Rimlinger, M. J., and Chyu, W. J., "Three- Dimensional Show-Wave/Boundary-Layer Interactions with Bleed," AIAA Journal, Vol. 31, No. 10, Oct. 1993, pp. 1819-1826.
    • (1993) AIAA Journal , vol.31 , Issue.10 , pp. 1819-1826
    • Shih, T.I.-P.1    Rimlinger, M.J.2    Chyu, W.J.3
  • 11
    • 0027595692 scopus 로고
    • Numerical Study of Shock-Wave/Boundary Interactions with Bleed
    • May
    • Hahn, T. O., Shih, T. I.-P., and Chyu, W. J., "Numerical Study of Shock-Wave/Boundary Interactions with Bleed," AIAA Journal, Vol. 31, No. 5, May 1993, pp. 869-876.
    • (1993) AIAA Journal , vol.31 , Issue.5 , pp. 869-876
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  • 12
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    • Harloff, G. J., and Smith, G. E., "Supersonic-Inlet Boundary-Layer Bleed Flow," AIAA Journal, Vol. 34, No. 4, April 1996, pp. 778-785.
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    • Harloff, G.J.1    Smith, G.E.2
  • 13
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    • Hypersonic Airbreathing Propulsion
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.