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Volumn 10, Issue 2, 2006, Pages 85-91

Unsteadiness in shock wave boundary layer interactions with separation

Author keywords

Shock induced separation; Shock unsteadiness; Three dimensional separation; Turbulent supersonic boundary layer

Indexed keywords

NATURAL FREQUENCIES; SEPARATION; SHOCK WAVES; SUPERSONIC AERODYNAMICS; TURBULENCE;

EID: 33644765831     PISSN: 12709638     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ast.2005.09.006     Document Type: Article
Times cited : (378)

References (43)
  • 1
    • 33644772639 scopus 로고    scopus 로고
    • Unsteadiness and side loads in overexpanded supersonic nozzles
    • 15-18 October 2001, Capua, Italy, ESA SP 487, March
    • T. Alziary de Roquefort, Unsteadiness and side loads in overexpanded supersonic nozzles, in: Proc. 4th Europ. Symp. Aerothermodynamics for Space Applications, 15-18 October 2001, Capua, Italy, ESA SP 487, March 2002
    • (2002) Proc. 4th Europ. Symp. Aerothermodynamics for Space Applications
    • De Roquefort, T.A.1
  • 2
    • 4243824682 scopus 로고
    • Characteristic frequency and length scales in transonic diffuser flows oscillations
    • AIAA Paper 81-1291, June 23-25
    • T.J. Bogar, M. Sajben, J.C. Kroutil, Characteristic frequency and length scales in transonic diffuser flows oscillations, in: 14th Fluid Plasma Dynamics Conference, AIAA Paper 81-1291, June 23-25 1981
    • (1981) 14th Fluid Plasma Dynamics Conference
    • Bogar, T.J.1    Sajben, M.2    Kroutil, J.C.3
  • 3
    • 33644754011 scopus 로고
    • Détermination des fluctuations de pression pariétale dans une interaction onde de choc-couche limite turbulente en écoulement supersonique
    • Convention ONERA 20.391/SAT.2.CDC, mai
    • J.P. Bonnet, E. Chaput, T. Alziary de Roquefort, Détermination des fluctuations de pression pariétale dans une interaction onde de choc-couche limite turbulente en écoulement supersonique, Rapport final, Convention ONERA 20.391/SAT.2.CDC, mai 1986
    • (1986) Rapport Final
    • Bonnet, J.P.1    Chaput, E.2    De Roquefort, T.A.3
  • 5
    • 27744481949 scopus 로고    scopus 로고
    • Experimental investigation of an unsteady and asymmetrical supersonic separated flow
    • Toronto, 29 April-2 May
    • A. Bourgoing, P.H. Reijasse, Experimental investigation of an unsteady and asymmetrical supersonic separated flow, in: CASI, 8th Aerodynamic Session Symposium, Toronto, 29 April-2 May 2001
    • (2001) CASI, 8th Aerodynamic Session Symposium
    • Bourgoing, A.1    Reijasse, P.H.2
  • 6
    • 0028482358 scopus 로고
    • Physics of unsteady blunt-fin-induced shock wave/turbulent boundary layer interaction
    • L. Brusniak, and D. Dolling Physics of unsteady blunt-fin-induced shock wave/turbulent boundary layer interaction Fluid Mech. 273 1994 375 409
    • (1994) Fluid Mech. , vol.273 , pp. 375-409
    • Brusniak, L.1    Dolling, D.2
  • 7
    • 0141630923 scopus 로고
    • Investigation of a separated flow in supersonic and subsonic streams with emphasis on the effect of transition
    • D.R. Chapman, D.M. Kuehn, H.K. Larson, Investigation of a separated flow in supersonic and subsonic streams with emphasis on the effect of transition, NACA TN-3869, 1957
    • (1957) NACA TN-3869
    • Chapman, D.R.1    Kuehn, D.M.2    Larson, H.K.3
  • 8
    • 0018529316 scopus 로고
    • Shock wave oscillations in a transonic diffuser flow
    • C.P. Chen, M. Sajben, and J.C. Krouttil Shock wave oscillations in a transonic diffuser flow AIAA J. 17 10 1979 1076 1083
    • (1979) AIAA J. , vol.17 , Issue.10 , pp. 1076-1083
    • Chen, C.P.1    Sajben, M.2    Krouttil, J.C.3
  • 9
    • 77951011978 scopus 로고
    • Pressure fluctuations underlying attached and separated supersonic turbulent boundary layers and shock waves
    • AIAA Paper 73-996, Seattle, WA, October 15-17
    • C.F. Coe, W.J. Chyu, J.B. Dods Jr., Pressure fluctuations underlying attached and separated supersonic turbulent boundary layers and shock waves, in: AIAA Aeroacoustics Conference, AIAA Paper 73-996, Seattle, WA, October 15-17, 1973
    • (1973) AIAA Aeroacoustics Conference
    • Coe, C.F.1    Chyu, W.J.2    Dods Jr., J.B.3
  • 10
    • 0020840766 scopus 로고
    • The response of normal shocks in diffusers
    • F.E.C. Culick, and T. Rogers The response of normal shocks in diffusers AIAA J. 21 10 1983 1382 1390
    • (1983) AIAA J. , vol.21 , Issue.10 , pp. 1382-1390
    • Culick, F.E.C.1    Rogers, T.2
  • 13
    • 0003565787 scopus 로고    scopus 로고
    • Shock wave - Boundary layer interactions
    • NATO, Neuilly s/Seine, France
    • o 280, NATO, Neuilly s/Seine, France
    • o 280 , vol.280
    • Delery, J.1    Marvin, G.J.2
  • 16
    • 85006373191 scopus 로고
    • Spatial and temporal features of a separated flow field at a convex wall induced by normal shock wave turbulent boundary layer interaction
    • Seattle, June
    • P. Doerffer, D.L.R. Dallmann, Spatial and temporal features of a separated flow field at a convex wall induced by normal shock wave turbulent boundary layer interaction, in: AIAA 21st Fluid Dynamics, Plasma Dynamics and Lasers Conference, Seattle, June 1990
    • (1990) AIAA 21st Fluid Dynamics, Plasma Dynamics and Lasers Conference
    • Doerffer, P.1    Dallmann, D.L.R.2
  • 17
    • 33644782857 scopus 로고    scopus 로고
    • Shock wave- boundary layer interaction control by streamwise vortices
    • Warsaw, Poland, 15-21 August
    • P. Doerffer, R. Szwaba, Shock wave- boundary layer interaction control by streamwise vortices, in: 11th ICTAM Symposium, Warsaw, Poland, 15-21 August 2004
    • (2004) 11th ICTAM Symposium
    • Doerffer, P.1    Szwaba, R.2
  • 18
    • 0035421035 scopus 로고    scopus 로고
    • Fifty years of shock wave/boundary layer interaction research: What next?
    • D.S. Dolling Fifty years of shock wave/boundary layer interaction research: what next? AIAA J. 39 8 2001
    • (2001) AIAA J. , vol.39 , Issue.8
    • Dolling, D.S.1
  • 19
    • 0024673746 scopus 로고
    • Separation shock motion in fin, cylinder, and compression ramp-induced turbulent interactions
    • D.S. Dolling, and L. Brusniak Separation shock motion in fin, cylinder, and compression ramp-induced turbulent interactions AIAA J. 27 6 1989
    • (1989) AIAA J. , vol.27 , Issue.6
    • Dolling, D.S.1    Brusniak, L.2
  • 20
    • 0021851683 scopus 로고
    • Unsteadiness of the shock wave structure in attached and separated compression ramp flows
    • D.S. Dolling, and C.T. Or Unsteadiness of the shock wave structure in attached and separated compression ramp flows Experiments in Fluids 3 24-32 1985
    • (1985) Experiments in Fluids , vol.3 , Issue.24-32
    • Dolling, D.S.1    Or, C.T.2
  • 21
    • 0024884882 scopus 로고
    • Unsteady shock-induced separation in Mach 5 cylinder interactions
    • D.S. Dolling, and D.R. Smith Unsteady shock-induced separation in Mach 5 cylinder interactions AIAA J. 27 12 1989 1598 1706
    • (1989) AIAA J. , vol.27 , Issue.12 , pp. 1598-1706
    • Dolling, D.S.1    Smith, D.R.2
  • 22
    • 33644779875 scopus 로고    scopus 로고
    • Space and time organization of a shock wave/turbulent boundary layer interaction
    • Paris, 22-24 mars Aerospace Science and Technology, submitted for publication
    • P. Dupont, C. Haddad, J.P. Ardissone, J.F. Debieve, Space and time organization of a shock wave/turbulent boundary layer interaction, in: 39ème colloque d'aérodynamique appliquée, Paris, 22-24 mars 2004, Aerospace Science and Technology, submitted for publication
    • (2004) 39ème Colloque d'Aérodynamique Appliquée
    • Dupont, P.1    Haddad, C.2    Ardissone, J.P.3    Debieve, J.F.4
  • 24
    • 0026156652 scopus 로고
    • Unsteady wave structure near separation in a Mach 5 compression ramp interaction
    • M.E. Erengil, and D.S. Dolling Unsteady wave structure near separation in a Mach 5 compression ramp interaction AIAA J. 29 5 1991
    • (1991) AIAA J. , vol.29 , Issue.5
    • Erengil, M.E.1    Dolling, D.S.2
  • 26
    • 33644784977 scopus 로고    scopus 로고
    • Etude de l'interaction de l'oscillation forcée d'une onde de choc avec une couche-limite décollée
    • A.A.A.F., Toulouse 21-23 mars
    • A. Galli, R. Bur, Etude de l'interaction de l'oscillation forcée d'une onde de choc avec une couche-limite décollée, in: 4ème Coll d'Aéro. Appl., A.A.A.F., Toulouse 21-23 mars 2005
    • (2005) 4ème Coll d'Aéro. Appl.
    • Galli, A.1    Bur, R.2
  • 28
    • 0036804619 scopus 로고    scopus 로고
    • Large eddy simulation of shock/boundary layer interaction
    • E. Garnier, and P. Sagaut Large eddy simulation of shock/boundary layer interaction AIAA J. 40 10 2002
    • (2002) AIAA J. , vol.40 , Issue.10
    • Garnier, E.1    Sagaut, P.2
  • 30
    • 0020865261 scopus 로고
    • Structure of a turbulent separation bubble
    • M. Kiya, and K. Sasaki Structure of a turbulent separation bubble J. Fluid Mech. 137 1983 83 113
    • (1983) J. Fluid Mech. , vol.137 , pp. 83-113
    • Kiya, M.1    Sasaki, K.2
  • 31
    • 0037328738 scopus 로고    scopus 로고
    • Advance in CFD prediction of shock wave turbulent boundary layer interactions
    • D. Knight, Y. Hong, A.G. Panaras, and A. Zheltovodov Advance in CFD prediction of shock wave turbulent boundary layer interactions Progr. Aerospace Sci. 39 2003 121 184
    • (2003) Progr. Aerospace Sci. , vol.39 , pp. 121-184
    • Knight, D.1    Hong, Y.2    Panaras, A.G.3    Zheltovodov, A.4
  • 32
    • 0035245485 scopus 로고    scopus 로고
    • Self-sustained shock oscillation on airfoils at transonic speeds
    • B.H.K. Lee Self-sustained shock oscillation on airfoils at transonic speeds Progr. Aerospace Sci. 37 2001 147 196
    • (2001) Progr. Aerospace Sci. , vol.37 , pp. 147-196
    • Lee, B.H.K.1
  • 38
    • 0035322272 scopus 로고    scopus 로고
    • Critical interaction of a shock wave with an acoustic wave
    • J.C. Robinet, and G. Casalis Critical interaction of a shock wave with an acoustic wave Phys. Fluids 13 4 2001
    • (2001) Phys. Fluids , vol.13 , Issue.4
    • Robinet, J.C.1    Casalis, G.2
  • 39
    • 0033115118 scopus 로고    scopus 로고
    • Shock oscillations in diffuser modeled by a selective noise amplification
    • J.C. Robinet, and G. Casalis Shock oscillations in diffuser modeled by a selective noise amplification AIAA J. 37 4 1999 453 459
    • (1999) AIAA J. , vol.37 , Issue.4 , pp. 453-459
    • Robinet, J.C.1    Casalis, G.2
  • 40
    • 0033842157 scopus 로고    scopus 로고
    • Shock wave instability and the carbuncle phenomenon: Same intrinsic origin
    • J.C. Robinet, J. Gressier, J.L. Moschetta, and G. Casalis Shock wave instability and the carbuncle phenomenon: same intrinsic origin J. Fluid Mech. 417 2000 237 263
    • (2000) J. Fluid Mech. , vol.417 , pp. 237-263
    • Robinet, J.C.1    Gressier, J.2    Moschetta, J.L.3    Casalis, G.4
  • 41
    • 0019634239 scopus 로고
    • Effect of initial boundary layer thickness on transonic diffuser flow
    • M. Sajben, and J.C. Kroutil Effect of initial boundary layer thickness on transonic diffuser flow AIAA J. 19 11 1981
    • (1981) AIAA J. , vol.19 , Issue.11
    • Sajben, M.1    Kroutil, J.C.2
  • 42
    • 0018479027 scopus 로고
    • Detailed study of attached and separated compression corner flowfields in high Reynolds number supersonic flow
    • G.S. Settle, T.J. Fitzpatrick, and S.M. Bogdonoff Detailed study of attached and separated compression corner flowfields in high Reynolds number supersonic flow AIAA J. 17 1979 579 585
    • (1979) AIAA J. , vol.17 , pp. 579-585
    • Settle, G.S.1    Fitzpatrick, T.J.2    Bogdonoff, S.M.3
  • 43
    • 0028736052 scopus 로고
    • On the mechanism of unsteady shock oscillation in shock wave/turbulent boundary layer interaction
    • P.O. Thomas, C.M. Putman, and H.C. Chu On the mechanism of unsteady shock oscillation in shock wave/turbulent boundary layer interaction Experiments in Fluids 18 1994 69 81
    • (1994) Experiments in Fluids , vol.18 , pp. 69-81
    • Thomas, P.O.1    Putman, C.M.2    Chu, H.C.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.