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Volumn 24, Issue 5, 2012, Pages

The three-dimensional flow organization past a micro-ramp in a supersonic boundary layer

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC STREAMING; ATMOSPHERIC THERMODYNAMICS; BOUNDARY LAYER FLOW; BOUNDARY LAYERS; COMPUTATIONAL FLUID DYNAMICS; REYNOLDS NUMBER; SHEAR FLOW; VELOCITY MEASUREMENT; VORTICITY; WAKES;

EID: 84861966501     PISSN: 10706631     EISSN: None     Source Type: Journal    
DOI: 10.1063/1.4711372     Document Type: Article
Times cited : (70)

References (29)
  • 1
    • 0021937157 scopus 로고
    • Shock wave/turbulent boundary layer interaction and its control
    • 10.1016/0376-0421(85)90001-6
    • Delery J.M. Shock wave/turbulent boundary layer interaction and its control. Prog. Aerosp. Sci. 1985, 22:209. 10.1016/0376-0421(85)90001-6
    • (1985) Prog. Aerosp. Sci. , vol.22 , pp. 209
    • Delery, J.M.1
  • 2
    • 0036588638 scopus 로고    scopus 로고
    • Review of research on low-profile vortex generators to control boundary-layer separation
    • 10.1016/S0376-0421(02)00010-6
    • Lin J.C. Review of research on low-profile vortex generators to control boundary-layer separation. Prog. Aerosp. Sci. 2002, 38:389. 10.1016/S0376-0421(02)00010-6
    • (2002) Prog. Aerosp. Sci. , vol.38 , pp. 389
    • Lin, J.C.1
  • 3
    • 84861994500 scopus 로고    scopus 로고
    • VGs for a normal SBLI with a downstream diffuser
    • AIAA Paper No. 2010-4464.
    • Rybalko M. Babinsky H. Loth E. VGs for a normal SBLI with a downstream diffuser. 2010 AIAA Paper No. 2010-4464.
    • (2010)
    • Rybalko, M.1    Babinsky, H.2    Loth, E.3
  • 4
    • 29544442462 scopus 로고    scopus 로고
    • Vortex-generator model and its application to flow control
    • 10.2514/1.12220
    • Jirasek A. Vortex-generator model and its application to flow control. J. Aircr. 2005, 42:1486. 10.2514/1.12220
    • (2005) J. Aircr. , vol.42 , pp. 1486
    • Jirasek, A.1
  • 5
    • 33845270733 scopus 로고    scopus 로고
    • Passive flow control on civil aircraft flaps using sub-boundary layer vortex generators in the AWIATOR programme
    • AIAA Paper No. 2006-2858.
    • Bohannon K.S. Passive flow control on civil aircraft flaps using sub-boundary layer vortex generators in the AWIATOR programme. 2006, AIAA Paper No. 2006-2858.
    • (2006)
    • Bohannon, K.S.1
  • 6
    • 84861989556 scopus 로고    scopus 로고
    • Preliminary numerical investigation of a Mach 3 inlet configuration with and without aspiration and micro-ramps
    • AIAA Paper No. 2010-1095.
    • Galbraith D.S. Galbraith M.C. Turner M.G. Orkwis P.D. Apyan A. Preliminary numerical investigation of a Mach 3 inlet configuration with and without aspiration and micro-ramps. 2010 AIAA Paper No. 2010-1095.
    • (2010)
    • Galbraith, D.S.1    Galbraith, M.C.2    Turner, M.G.3    Orkwis, P.D.4    Apyan, A.5
  • 7
    • 35649023593 scopus 로고    scopus 로고
    • Optimal control of shock wave turbulent boundary layer interactions using micro-array actuation
    • AIAA Paper No. 2006-3197.
    • Anderson B.H. Tinapple H. Surber L. Optimal control of shock wave turbulent boundary layer interactions using micro-array actuation. 2006 AIAA Paper No. 2006-3197.
    • (2006)
    • Anderson, B.H.1    Tinapple, H.2    Surber, L.3
  • 8
    • 78649886905 scopus 로고    scopus 로고
    • Experimental investigation of the application of microramp flow control to an oblique shock interaction
    • AIAA Paper No. 2006-3197.
    • Hirt S.M. Anderson B.H. Experimental investigation of the application of microramp flow control to an oblique shock interaction. 2006 AIAA Paper No. 2006-3197.
    • (2006)
    • Hirt, S.M.1    Anderson, B.H.2
  • 9
    • 78650402536 scopus 로고    scopus 로고
    • Micro-ramp flow control of normal shock/boundary layer interactions
    • 10.2514/1.J050313
    • Herges T. Kroeker E. Elliott G. Dutton C. Micro-ramp flow control of normal shock/boundary layer interactions. AIAA J. 2010, 48:2529. 10.2514/1.J050313.
    • (2010) AIAA J. , vol.48 , pp. 2529
    • Herges, T.1    Kroeker, E.2    Elliott, G.3    Dutton, C.4
  • 10
    • 77049090026 scopus 로고    scopus 로고
    • Microramps upstreams of an oblique-shock/boundary-layer interaction
    • 10.2514/1.41776
    • Lee S. Goettke M.K. Loth E. Microramps upstreams of an oblique-shock/boundary-layer interaction. AIAA J. 2010, 48:104. 10.2514/1.41776.
    • (2010) AIAA J. , vol.48 , pp. 104
    • Lee, S.1    Goettke, M.K.2    Loth, E.3
  • 11
    • 78649878886 scopus 로고    scopus 로고
    • LES for supersonic ramp control flow using MVG at M = 2.5 and Reθ = 1440
    • AIAA Paper No. 2010-592.
    • Li Q. Liu C. LES for supersonic ramp control flow using MVG at M = 2.5 and Reθ = 1440. 2010 AIAA Paper No. 2010-592.
    • (2010)
    • Li, Q.1    Liu, C.2
  • 12
    • 78751507045 scopus 로고    scopus 로고
    • Effect on Mach number on flow past microramps
    • 10.2514/1.J050267
    • Lee S. Loth E. Georgiadis N.J. DeBonis J.R. Effect on Mach number on flow past microramps. AIAA J. 2011, 49:97. 10.2514/1.J050267.
    • (2011) AIAA J. , vol.49 , pp. 97
    • Lee, S.1    Loth, E.2    Georgiadis, N.J.3    DeBonis, J.R.4
  • 13
    • 74549159666 scopus 로고    scopus 로고
    • Supersonic boundary-layer interactions with various micro-vortex generator geometries
    • Lee S. Loth E. Supersonic boundary-layer interactions with various micro-vortex generator geometries. Aeronaut. J. 2009, 113:683
    • (2009) Aeronaut. J. , vol.113 , pp. 683
    • Lee, S.1    Loth, E.2
  • 14
    • 79251475272 scopus 로고    scopus 로고
    • Numerical investigations on the effects of the declining angle of the trailing-edge of MVG
    • 10.2514/1.C000318
    • Li Q. Liu C. Numerical investigations on the effects of the declining angle of the trailing-edge of MVG. J. Aircr. 2010, 47:2086. 10.2514/1.C000318.
    • (2010) J. Aircr. , vol.47 , pp. 2086
    • Li, Q.1    Liu, C.2
  • 15
    • 62149091794 scopus 로고    scopus 로고
    • Microramp control of supersonic oblique shock-wave/boundary-layer interactions
    • 10.2514/1.38022
    • Babinsky H. Li Y. Pitt Ford C.W. Microramp control of supersonic oblique shock-wave/boundary-layer interactions. Aeronaut. J. 2009, 47:668. 10.2514/1.38022.
    • (2009) Aeronaut. J. , vol.47 , pp. 668
    • Babinsky, H.1    Li, Y.2    Pitt Ford, C.W.3
  • 16
    • 71149114454 scopus 로고    scopus 로고
    • Effects of micro-ramps on a shock wave/turbulent boundary layer interaction
    • 10.1007/s00193-009-0231-9
    • Blinde P.L. Humble R.A. van Oudheusden B.W. Scarano F. Effects of micro-ramps on a shock wave/turbulent boundary layer interaction. Shock Waves 2009, 19:507. 10.1007/s00193-009-0231-9.
    • (2009) Shock Waves , vol.19 , pp. 507
    • Blinde, P.L.1    Humble, R.A.2    van Oudheusden, B.W.3    Scarano, F.4
  • 17
    • 79953733641 scopus 로고    scopus 로고
    • Experimental study of near wake of micro vortex generators in supersonic flow
    • AIAA Paper No. 2010-4623.
    • Lu F.K. Pierce A.J. Shih Y. Experimental study of near wake of micro vortex generators in supersonic flow. 2010 AIAA Paper No. 2010-4623.
    • (2010)
    • Lu, F.K.1    Pierce, A.J.2    Shih, Y.3
  • 18
    • 0027606721 scopus 로고
    • The flow structure and statistics of a passive mixing tab
    • 10.1115/1.2910133
    • Gretta W.J. Smith C.R. The flow structure and statistics of a passive mixing tab. J. Fluids Eng. 1993, 115:255. 10.1115/1.2910133.
    • (1993) J. Fluids Eng. , vol.115 , pp. 255
    • Gretta, W.J.1    Smith, C.R.2
  • 19
    • 0035357635 scopus 로고    scopus 로고
    • Dynamics of hairpin vortices generated by a mixing tab in a channel flow
    • 10.1007/s003480000252
    • Yang W. Meng H. Sheng J. Dynamics of hairpin vortices generated by a mixing tab in a channel flow. Exp. Fluids 2001, 30:705. 10.1007/s003480000252.
    • (2001) Exp. Fluids , vol.30 , pp. 705
    • Yang, W.1    Meng, H.2    Sheng, J.3
  • 21
    • 77952401136 scopus 로고    scopus 로고
    • Three-dimensional vortex organization in a high-Reynolds-number supersonic turbulent boundary layer
    • 10.1017/S0022112009992047
    • Elsinga G.E. Adrain R.J. van Oudheusden B.W. Scarano F. Three-dimensional vortex organization in a high-Reynolds-number supersonic turbulent boundary layer. J. Fluid Mech. 2010, 644:35. 10.1017/S0022112009992047.
    • (2010) J. Fluid Mech. , vol.644 , pp. 35
    • Elsinga, G.E.1    Adrain, R.J.2    van Oudheusden, B.W.3    Scarano, F.4
  • 22
    • 65649104740 scopus 로고    scopus 로고
    • Three-dimensional instantaneous structure of a shock wave/turbulent boundary layer interaction
    • 10.1017/S0022112008005090
    • Humble R.A. Elsinga G.E. Scarano F. van Oudheusden B.W. Three-dimensional instantaneous structure of a shock wave/turbulent boundary layer interaction. J. Fluid Mech. 2009, 622:33. 10.1017/S0022112008005090.
    • (2009) J. Fluid Mech. , vol.622 , pp. 33
    • Humble, R.A.1    Elsinga, G.E.2    Scarano, F.3    van Oudheusden, B.W.4
  • 23
    • 34548067721 scopus 로고    scopus 로고
    • Particle image velocimetry measurement of a shock wave/turbulent boundary layer interaction
    • 10.1007/s00348-007-0337-8
    • Humble R.A. Scarano F. Oudheusden B.W. Particle image velocimetry measurement of a shock wave/turbulent boundary layer interaction. Exp. Fluids 2007, 43:173. 10.1007/s00348-007-0337-8.
    • (2007) Exp. Fluids , vol.43 , pp. 173
    • Humble, R.A.1    Scarano, F.2    Oudheusden, B.W.3
  • 24
    • 79751534442 scopus 로고    scopus 로고
    • Particle tracer response across shocks measured by PIV
    • 10.1007/s00348-010-0892-2
    • Ragni D. Schrijer F.F. J. van Oudheusden B.W. Scarano F. Particle tracer response across shocks measured by PIV. Exp. Fluids 2011, 50:53. 10.1007/s00348-010-0892-2.
    • (2011) Exp. Fluids , vol.50 , pp. 53
    • Ragni, D.1    Schrijer, F.F.J.2    van Oudheusden, B.W.3    Scarano, F.4
  • 25
    • 54249114598 scopus 로고    scopus 로고
    • Effect of predictor-corrector filtering on the stability and spatial resolution of iterative PIV interrogation
    • 10.1007/s00348-008-0511-7
    • Schrijer F.F. J. Scarano F. Effect of predictor-corrector filtering on the stability and spatial resolution of iterative PIV interrogation. Exp. Fluids 2008, 45:927. 10.1007/s00348-008-0511-7.
    • (2008) Exp. Fluids , vol.45 , pp. 927
    • Schrijer, F.F.J.1    Scarano, F.2
  • 26
    • 1942461062 scopus 로고    scopus 로고
    • Flow past a trapezoidal tab
    • 10.1017/S0022112004009486
    • Dong S. Meng H. Flow past a trapezoidal tab. J. Fluid Mech. 2004, 510:219. 10.1017/S0022112004009486.
    • (2004) J. Fluid Mech. , vol.510 , pp. 219
    • Dong, S.1    Meng, H.2
  • 27
    • 78649963783 scopus 로고    scopus 로고
    • Experimental and numerical study of flow topology past micro vortex generators
    • AIAA Paper No. 2010-4463.
    • Lu F.K. Pierce A.J. Shih Y. Liu C. Li Q. Experimental and numerical study of flow topology past micro vortex generators. 2010 AIAA Paper No. 2010-4463.
    • (2010)
    • Lu, F.K.1    Pierce, A.J.2    Shih, Y.3    Liu, C.4    Li, Q.5
  • 28
    • 0033865011 scopus 로고    scopus 로고
    • Flow visualization study of the role of coherent structures in a tab wake
    • 10.1016/S0169-5983(00)00003-4
    • Elavarasan R. Meng H. Flow visualization study of the role of coherent structures in a tab wake. Fluid Dyn. Res. 2000, 27:183. 10.1016/S0169-5983(00)00003-4.
    • (2000) Fluid Dyn. Res. , vol.27 , pp. 183
    • Elavarasan, R.1    Meng, H.2
  • 29
    • 84881449566 scopus 로고    scopus 로고
    • The interaction between vortex rings and oblique shocks by the MVG controlled ramp flow at M = 2.5
    • AIAA Paper No. 2011-861.
    • Li Q. Yang Y. Wang X. Liu C. The interaction between vortex rings and oblique shocks by the MVG controlled ramp flow at M = 2.5. 2011 AIAA Paper No. 2011-861.
    • (2011)
    • Li, Q.1    Yang, Y.2    Wang, X.3    Liu, C.4


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.