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Volumn 14, Issue , 2006, Pages 10486-10497

Experimental investigation of 3D shock / boundary layer interaction control in transonic flows

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; DRAG REDUCTION; FLOW VISUALIZATION; PRESSURE MEASUREMENT; TRANSONIC FLOW; WIND TUNNELS;

EID: 34250730718     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2006-879     Document Type: Conference Paper
Times cited : (6)

References (22)
  • 1
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    • Shock Wave / Boundary Layer Interaction and its Control
    • 1095, pp
    • Délery,J., "Shock Wave / Boundary Layer Interaction and its Control", Progress in Aerospace Sciences, vol.22, No.4, 1095, pp.209-280
    • Progress in Aerospace Sciences , vol.22 , Issue.4 , pp. 209-280
    • Délery, J.1
  • 4
    • 13844281243 scopus 로고    scopus 로고
    • Separated Shock-Boundary-Layer Interaction Control Using Streamwise Slots
    • Holden,H.A. and Babinsky,H., "Separated Shock-Boundary-Layer Interaction Control Using Streamwise Slots", Journal of Aircraft, vol.42, No.1, 2005, pp.166-171
    • (2005) Journal of Aircraft , vol.42 , Issue.1 , pp. 166-171
    • Holden, H.A.1    Babinsky, H.2
  • 7
    • 3042718258 scopus 로고    scopus 로고
    • Shock-Wave / Boundary-Layer Interaction Control Using Streamwise Slots in Transonic Flows
    • Smith,A.N., Babinsky,H., Fulker,J., Ashill,P.R., "Shock-Wave / Boundary-Layer Interaction Control Using Streamwise Slots in Transonic Flows", Journal of Aircraft, vol.41, No.3, 2004, pp.540-546
    • (2004) Journal of Aircraft , vol.41 , Issue.3 , pp. 540-546
    • Smith, A.N.1    Babinsky, H.2    Fulker, J.3    Ashill, P.R.4
  • 10
    • 11644312718 scopus 로고    scopus 로고
    • The formation and evolution of synthetic jets
    • Smith,B.L. and Glezer,A., "The formation and evolution of synthetic jets", Physics of Fluids, vol.10, No.9, 1998, pp.2281-2297
    • (1998) Physics of Fluids , vol.10 , Issue.9 , pp. 2281-2297
    • Smith, B.L.1    Glezer, A.2
  • 11
    • 34250705605 scopus 로고    scopus 로고
    • 11Stanewsky,E., Delery,J., Fulker,J.L. and de Matteis,P., EUROSHOCK II - Drag Reduction by Shock and Boundary Layer Control, Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 80, 2002
    • 11Stanewsky,E., Delery,J., Fulker,J.L. and de Matteis,P., "EUROSHOCK II - Drag Reduction by Shock and Boundary Layer Control", Notes on Numerical Fluid Mechanics and Multidisciplinary Design, vol.80, 2002
  • 13
    • 30744466435 scopus 로고    scopus 로고
    • Evaluation of Wave Drag Reduction by Flow Control
    • AIAA Paper 2005-1415
    • Ogawa,H. and Babinsky,H., "Evaluation of Wave Drag Reduction by Flow Control", AIAA Paper 2005-1415, 2005
    • (2005)
    • Ogawa, H.1    Babinsky, H.2
  • 15
    • 0347354887 scopus 로고    scopus 로고
    • Shock wave - boundary layer interaction control by wall ventilation
    • Doerffer,P. and Bohning,R., "Shock wave - boundary layer interaction control by wall ventilation", Aerospace Science and Technology, vol.7, No.3, 2003, pp.171-179
    • (2003) Aerospace Science and Technology , vol.7 , Issue.3 , pp. 171-179
    • Doerffer, P.1    Bohning, R.2
  • 16
    • 33751222307 scopus 로고    scopus 로고
    • Transonic Shock / Boundary Layer Interaction Control Using Three-dimensional Devices
    • PhD dissertation, University of Cambridge
    • Holden,H.A., "Transonic Shock / Boundary Layer Interaction Control Using Three-dimensional Devices", PhD dissertation, University of Cambridge, 2004
    • (2004)
    • Holden, H.A.1
  • 19
    • 34250775835 scopus 로고    scopus 로고
    • Seddon,J., The flow produced by interaction of a turbulent boundary layer with a normal shock of strength sufficient to cause separation, ARC R and M 3502, 1960
    • Seddon,J., "The flow produced by interaction of a turbulent boundary layer with a normal shock of strength sufficient to cause separation", ARC R and M 3502, 1960
  • 20
    • 34250703509 scopus 로고    scopus 로고
    • Kooi,J.W., Influence of Free-stream Mach Number on Transonic Shock-wave Boundary-layer Interaction, NLR MP 78013 U, 1978
    • Kooi,J.W., "Influence of Free-stream Mach Number on Transonic Shock-wave Boundary-layer Interaction", NLR MP 78013 U, 1978
  • 21
    • 0027150227 scopus 로고
    • Shock / Boundary-Layer Interaction Control with Vortex Generators and Passive Cavity
    • McCormick,D.C., "Shock / Boundary-Layer Interaction Control with Vortex Generators and Passive Cavity", AIAA Journal, vol.31, No.1, 1993, pp.91-96
    • (1993) AIAA Journal , vol.31 , Issue.1 , pp. 91-96
    • McCormick, D.C.1
  • 22
    • 0033698843 scopus 로고    scopus 로고
    • Passive control of shock wave-boundary layer interactions
    • Gibson,T.M., Babinsky,H. and Squire,L.C., "Passive control of shock wave-boundary layer interactions", The Aeronautical Journal, vol.104, No.3, 2000, pp. 129-140
    • (2000) The Aeronautical Journal , vol.104 , Issue.3 , pp. 129-140
    • Gibson, T.M.1    Babinsky, H.2    Squire, L.C.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.