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Volumn 31, Issue 1, 1993, Pages 8-9

Three-dimensional hypersonic shock wave/turbulent boundary-layer interactions

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYER FLOW; FLOW INTERACTIONS; FRICTION; HEAT TRANSFER; MATHEMATICAL MODELS; PRESSURE EFFECTS; SHOCK WAVES; TURBULENT FLOW;

EID: 0027148445     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.11310     Document Type: Article
Times cited : (10)

References (6)
  • 1
    • 0003217388 scopus 로고
    • Swept Shock/Boundary-Layer Interactions—Tutorial and Update
    • Jan
    • Settles, G. S., and Dolling, D. S., “Swept Shock/Boundary-Layer Interactions—Tutorial and Update,” AIAA Paper 90-0375, Jan. 1990.
    • (1990) AIAA Paper 90-0375
    • Settles, G.S.1    Dolling, D.S.2
  • 2
    • 85006741688 scopus 로고
    • Hypersonic Shock/Boundary Layer Interaction Database
    • June
    • Settles, G. S., and Dodson, L. J., “Hypersonic Shock/Boundary Layer Interaction Database,” AIAA Paper 91-1763, June 1991;
    • (1991) AIAA Paper 91-1763
    • Settles, G.S.1    Dodson, L.J.2
  • 4
    • 85002902831 scopus 로고
    • An Experimental Study of a Three-Dimensional Shock Wave/Turbulent Boundary-Layer Interaction at a Hypersonic Mach Number
    • June
    • Kussoy, M. I., Kim, K. S., and Horstman, K. C., “An Experimental Study of a Three-Dimensional Shock Wave/Turbulent Boundary-Layer Interaction at a Hypersonic Mach Number,” AIAA Paper 91-1761, June 1991.
    • (1991) AIAA Paper 91-1761
    • Kussoy, M.I.1    Kim, K.S.2    Horstman, K.C.3
  • 5
    • 0013414345 scopus 로고
    • Documentation of Two-and Three-Dimensional Shock-Wave/Turbulent Boundary-Layer Interaction Flows at Mach 8.2
    • Kussoy, M. I., and Horstman, K. C., “Documentation of Two-and Three-Dimensional Shock-Wave/Turbulent Boundary-Layer Interaction Flows at Mach 8.2,” NASA TM 103838, May 1991.
    • (1991) NASA TM 103838
    • Kussoy, M.I.1    Horstman, K.C.2
  • 6
    • 85002644444 scopus 로고
    • The Hypersonic Shock Wave-Turbulent Boundary Layer Interaction Generated by a Sharp Fin at Mach 8.2
    • Jan
    • Knight, D. D., Horstman, C. C., and Monson, D. J., “The Hypersonic Shock Wave-Turbulent Boundary Layer Interaction Generated by a Sharp Fin at Mach 8.2,” AIAA Paper 92-0747, Jan. 1992.
    • (1992) AIAA Paper 92-0747
    • Knight, D.D.1    Horstman, C.C.2    Monson, D.J.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.