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Volumn 12, Issue 5, 2013, Pages 375-384

Development of some hypersonic benchmark flows using CFD and experiment

Author keywords

Benchmark cases; CFD; Experiment; Hypersonic

Indexed keywords


EID: 0346034635     PISSN: 09381287     EISSN: None     Source Type: Journal    
DOI: 10.1007/s00193-003-0179-0     Document Type: Article
Times cited : (10)

References (44)
  • 1
    • 0000054178 scopus 로고
    • Global stability of a lid-driven cavity with throughflow: Flow visualisation studies
    • Aidun CK, Triantafillopoulos NG, Benson JD (1991) Global stability of a lid-driven cavity with throughflow: flow visualisation studies. Phys Fluids A3:2081-2093
    • (1991) Phys Fluids , vol.A3 , pp. 2081-2093
    • Aidun, C.K.1    Triantafillopoulos, N.G.2    Benson, J.D.3
  • 2
    • 84988012990 scopus 로고    scopus 로고
    • Baldwin BS, Barth TJ (1990) A one-equation turbulence model for high Reynolds number wall bounded flows. NASA TM102847
  • 3
    • 84988040586 scopus 로고    scopus 로고
    • Baldwin BS, Lomax H (1978) Thin layer approximation and algebraic model for separated turbulent flows. AIAA78-257
  • 4
    • 84987935418 scopus 로고    scopus 로고
    • Boyce RR, Hillier R (2000) Shock-induced three-dimensional separation of an axisymmetric hypersonic turbulent boundary layer. AIAA 2000-2226
  • 5
    • 0023849835 scopus 로고
    • Two-component LDV investigation of three-dimensional shock/turbulent boundary-layer interactions
    • Brown JD, Brown JL, Kussoy MI, Holt M, Horstman CC (1988) Two-component LDV investigation of three-dimensional shock/turbulent boundary-layer interactions. AIAA J 26:52-56
    • (1988) AIAA J , vol.26 , pp. 52-56
    • Brown, J.D.1    Brown, J.L.2    Kussoy, M.I.3    Holt, M.4    Horstman, C.C.5
  • 6
    • 85007670845 scopus 로고
    • Reduction of data from thin-film heat-transfer gauges: A concise numerical technique
    • Cook WJ, Felderman EJ (1966) Reduction of data from thin-film heat-transfer gauges: a concise numerical technique. AIAA J 4:561-562
    • (1966) AIAA J , vol.4 , pp. 561-562
    • Cook, W.J.1    Felderman, E.J.2
  • 7
    • 0027927471 scopus 로고
    • The structure of a supersonic turbulent boundary layer subjected to concave surface curvature
    • Donovan JF, Spina EF, Smits AJ (1994) The structure of a supersonic turbulent boundary layer subjected to concave surface curvature. J Fluid Mech 259:1-24
    • (1994) J Fluid Mech , vol.259 , pp. 1-24
    • Donovan, J.F.1    Spina, E.F.2    Smits, A.J.3
  • 8
    • 0035421035 scopus 로고    scopus 로고
    • Fifty years of shock-wave/boundary layer interaction research: What next?
    • Dolling DS (2001) Fifty years of shock-wave/boundary layer interaction research: What next? AIAA J 39:1517-1531
    • (2001) AIAA J , vol.39 , pp. 1517-1531
    • Dolling, D.S.1
  • 9
    • 0025387940 scopus 로고
    • A supersonic turbulent boundary layer in an adverse pressure gradient
    • Fernando EM, Smits AJ (1990) A supersonic turbulent boundary layer in an adverse pressure gradient. J Fluid Mech 211:285-307
    • (1990) J Fluid Mech , vol.211 , pp. 285-307
    • Fernando, E.M.1    Smits, A.J.2
  • 10
    • 0031140862 scopus 로고    scopus 로고
    • Structure of a supersonic three-dimensional/offset-flare turbulent interaction
    • Gaitonde D, Shang JS, Edwards JR (1997) Structure of a supersonic three-dimensional/offset-flare turbulent interaction. AIAA J 34:294-302
    • (1997) AIAA J , vol.34 , pp. 294-302
    • Gaitonde, D.1    Shang, J.S.2    Edwards, J.R.3
  • 11
  • 12
    • 84912262813 scopus 로고
    • Concerning some solutions of the boundary layer equations in hydrodynamics
    • Goldstein S (1930) Concerning some solutions of the boundary layer equations in hydrodynamics. Proc Camb Phil Soc 26:18-30
    • (1930) Proc Camb Phil Soc , vol.26 , pp. 18-30
    • Goldstein, S.1
  • 13
    • 0001814922 scopus 로고    scopus 로고
    • Assessment of turbulence model performance for transonic flow over an axisymmetric bump
    • Hasan RGM, McGuirk JJ (2001) Assessment of turbulence model performance for transonic flow over an axisymmetric bump. Aero J 105:17-31
    • (2001) Aero J , vol.105 , pp. 17-31
    • Hasan, R.G.M.1    McGuirk, J.J.2
  • 15
    • 0000483682 scopus 로고
    • Establishment time of laminar separated flows
    • Holden M (1971) Establishment time of laminar separated flows. AIAA J 9:2296-2298
    • (1971) AIAA J , vol.9 , pp. 2296-2298
    • Holden, M.1
  • 16
    • 85003338235 scopus 로고
    • Quasi-steady aspects of the adjustment of separated flow regions to transient external flows
    • Ihrig HK, Korst HH (1963) Quasi-steady aspects of the adjustment of separated flow regions to transient external flows. AIAA J 1:934-937
    • (1963) AIAA J , vol.1 , pp. 934-937
    • Ihrig, H.K.1    Korst, H.H.2
  • 17
    • 0346981058 scopus 로고    scopus 로고
    • A study of two- and three-dimensional separation at hypersonic speeds
    • Ball GJ, Hillier R, Roberts GT, University of Southampton
    • Jackson AP, Hillier R, Soltani S (1999) A study of two- and three-dimensional separation at hypersonic speeds. In Ball GJ, Hillier R, Roberts GT 22nd Int. Symp. on Shock Waves, University of Southampton, pp 1571-1576
    • (1999) 22nd Int. Symp. on Shock Waves , pp. 1571-1576
    • Jackson, A.P.1    Hillier, R.2    Soltani, S.3
  • 18
    • 0035945543 scopus 로고    scopus 로고
    • Experimental and computational study of laminar cavity flows at hypersonic speeds
    • Jackson AP, Hillier R, Soltani S (2001) Experimental and computational study of laminar cavity flows at hypersonic speeds. J Fluid Mech 427:329-358
    • (2001) J Fluid Mech , vol.427 , pp. 329-358
    • Jackson, A.P.1    Hillier, R.2    Soltani, S.3
  • 19
    • 84987956750 scopus 로고    scopus 로고
    • Keyes FG (1952) The heat conductivity, viscosity, specific heat and Prandtl numbers for thirteen gases. Massachussetts Institute of Technology, Project Squid, Tech Report 37
  • 20
    • 0026850683 scopus 로고
    • Structure of supersonic turbulent flow past a swept compression corner
    • Knight DD, Horstman CC, Bogdonoff S (1992) Structure of supersonic turbulent flow past a swept compression corner. AIAA J 30:890-896
    • (1992) AIAA J , vol.30 , pp. 890-896
    • Knight, D.D.1    Horstman, C.C.2    Bogdonoff, S.3
  • 21
    • 84987935416 scopus 로고    scopus 로고
    • Kussoy MI, Horstman CC, Acharya M (1978) An experimental documentation of pressure gradient and Reynolds number effects on compressible turbulent boundary layers. NASA TM 78488
  • 22
    • 0019243789 scopus 로고
    • Investigation of a three-dimensional shock wave separated turbulent boundary layer
    • Kussoy MI, Viegas JR, Horstman CC (1980) Investigation of a three-dimensional shock wave separated turbulent boundary layer. AIAA J 18:1477-1484
    • (1980) AIAA J , vol.18 , pp. 1477-1484
    • Kussoy, M.I.1    Viegas, J.R.2    Horstman, C.C.3
  • 23
    • 0019075469 scopus 로고
    • Adverse pressure gradient effect on supersonic boundary layer turbulence
    • Laderman AJ (1980) Adverse pressure gradient effect on supersonic boundary layer turbulence. AIAA J 18:1186-1195,
    • (1980) AIAA J , vol.18 , pp. 1186-1195
    • Laderman, A.J.1
  • 24
    • 0031493507 scopus 로고    scopus 로고
    • Establishment of steady separated flow over a compression-corner in a free piston shock tunnel
    • Mallinson SG, Gai SL, Mudford NR (1997) Establishment of steady separated flow over a compression-corner in a free piston shock tunnel. Shock Waves 7:249-253
    • (1997) Shock Waves , vol.7 , pp. 249-253
    • Mallinson, S.G.1    Gai, S.L.2    Mudford, N.R.3
  • 25
    • 0346351174 scopus 로고    scopus 로고
    • Turbulence modelling of hypersonic turbulent boundary layer flows
    • Ball GJ, Hillier R, Roberts GT, University of Southampton
    • Mallinson SG, Hillier R, Jackson AP (1999) Turbulence modelling of hypersonic turbulent boundary layer flows. In Ball GJ, Hillier R, Roberts GT 22nd Int. Symp. on Shock Waves, University of Southampton, pp 1519-1524
    • (1999) 22nd Int. Symp. on Shock Waves , pp. 1519-1524
    • Mallinson, S.G.1    Hillier, R.2    Jackson, A.P.3
  • 27
    • 0031356558 scopus 로고    scopus 로고
    • Eddy viscosity transport equations and their relation to the k - ε model
    • Menter FR (1997) Eddy viscosity transport equations and their relation to the k - ε model. J Fluids Eng 119:876-884
    • (1997) J Fluids Eng , vol.119 , pp. 876-884
    • Menter, F.R.1
  • 28
    • 0028671320 scopus 로고
    • Hypersonic flow past open cavities
    • Morgenstern A, Chokani N (1994) Hypersonic flow past open cavities. AIAA J 32:2387-2393
    • (1994) AIAA J , vol.32 , pp. 2387-2393
    • Morgenstern, A.1    Chokani, N.2
  • 29
    • 84988012991 scopus 로고    scopus 로고
    • Oberkampf WL (2000) Design, execution and analysis of validation experiments. Verification and validation in CFD, VKI-lecture series
  • 30
    • 0029761838 scopus 로고    scopus 로고
    • Review of the physics of swept-shock/boundary layer interactions
    • Panaras AG (1996) Review of the physics of swept-shock/boundary layer interactions. Prog Aero Sci 37:173-244
    • (1996) Prog Aero Sci , vol.37 , pp. 173-244
    • Panaras, A.G.1
  • 31
    • 0022130944 scopus 로고
    • Turbulence models for near-wall and low Reynolds number flows: A review
    • Patel VC, Rodi W, Scheurer G (1985) Turbulence models for near-wall and low Reynolds number flows: a review. AIAA J 23:1308-1319
    • (1985) AIAA J , vol.23 , pp. 1308-1319
    • Patel, V.C.1    Rodi, W.2    Scheurer, G.3
  • 32
    • 0028112345 scopus 로고
    • Linear stability of lid-driven cavity flows
    • Ramanan N, Homsy GM (1994) Linear stability of lid-driven cavity flows. Phys Fluids 6:2690-2701
    • (1994) Phys Fluids , vol.6 , pp. 2690-2701
    • Ramanan, N.1    Homsy, G.M.2
  • 33
    • 0000489749 scopus 로고    scopus 로고
    • Towards establishing credibility in computational fluid dynamics simulations
    • Rizzi AW, Vos JB (1998) Towards establishing credibility in computational fluid dynamics simulations. AIAA Journal 36:668-675
    • (1998) AIAA Journal , vol.36 , pp. 668-675
    • Rizzi, A.W.1    Vos, J.B.2
  • 34
    • 85003264300 scopus 로고
    • Measurements of heat transfer in separated regions in a shock tube and in a shock tunnel
    • Rom J (1963) Measurements of heat transfer in separated regions in a shock tube and in a shock tunnel. AIAA J 1:2193-2194
    • (1963) AIAA J , vol.1 , pp. 2193-2194
    • Rom, J.1
  • 35
    • 85003365646 scopus 로고
    • Observations of turbulent reattachment behind an axisymmetric downstream-facing step in supersonic flow
    • Roshko A, Thomke GJ (1966) Observations of turbulent reattachment behind an axisymmetric downstream-facing step in supersonic flow. AIAA J 4:975-980
    • (1966) AIAA J , vol.4 , pp. 975-980
    • Roshko, A.1    Thomke, G.J.2
  • 36
    • 84865639176 scopus 로고
    • Heat-transfer measurements in short-duration hypersonic facilities
    • Schultz DL, Jones TV (1973) Heat-transfer measurements in short-duration hypersonic facilities, AGARDograph 165
    • (1973) AGARDograph , vol.165
    • Schultz, D.L.1    Jones, T.V.2
  • 37
    • 0022714202 scopus 로고
    • Experimental and computational study of a swept compression corner interaction flowfield
    • Settles GS, Horstman CC, McKenzie TM (1986) Experimental and computational study of a swept compression corner interaction flowfield. AIAA J 24:744-752
    • (1986) AIAA J , vol.24 , pp. 744-752
    • Settles, G.S.1    Horstman, C.C.2    McKenzie, T.M.3
  • 38
    • 0031222740 scopus 로고    scopus 로고
    • Compressibility effects in modeling complex turbulent flows
    • Shyy W, Krishnamurty VS (1997) Compressibility effects in modeling complex turbulent flows. Prog Aero Sci 33:587-645
    • (1997) Prog Aero Sci , vol.33 , pp. 587-645
    • Shyy, W.1    Krishnamurty, V.S.2
  • 39
    • 0029277793 scopus 로고    scopus 로고
    • A study of the effects of curvature and compression on the behavior of a supersonic turbulent boundary layer
    • Smith DR, Smits AJ (1996) A study of the effects of curvature and compression on the behavior of a supersonic turbulent boundary layer. Experiments in Fluids 18:363-369
    • (1996) Experiments in Fluids , vol.18 , pp. 363-369
    • Smith, D.R.1    Smits, A.J.2
  • 40
    • 3242836148 scopus 로고    scopus 로고
    • Algebraic turbulence model simulations of supersonic open-cavity flow physics
    • Tam C-J, Orkwis PD, Disimile PJ (1996) Algebraic turbulence model simulations of supersonic open-cavity flow physics. AIAA J 34:2255-2260
    • (1996) AIAA J , vol.34 , pp. 2255-2260
    • Tam, C.-J.1    Orkwis, P.D.2    Disimile, P.J.3
  • 41
    • 84987935407 scopus 로고    scopus 로고
    • Overview of European validation activities in aeronautics
    • Vos JB, Rizzi AW, Darracq D (2001) Overview of European validation activities in aeronautics. QNET-CFD Network Newsletter (http://www.qnet-cfd.net):17-20
    • (2001) QNET-CFD Network Newsletter , pp. 17-20
    • Vos, J.B.1    Rizzi, A.W.2    Darracq, D.3
  • 42
    • 0029104980 scopus 로고
    • Skin-friction measurements in three-dimensional shock-wave/boundary-layer interaction
    • Wideman JK, Brown JL, Miles JB, Ozcan O (1995) Skin-friction measurements in three-dimensional shock-wave/boundary-layer interaction. AIAA J 33:805-811
    • (1995) AIAA J , vol.33 , pp. 805-811
    • Wideman, J.K.1    Brown, J.L.2    Miles, J.B.3    Ozcan, O.4
  • 43
    • 84988012989 scopus 로고    scopus 로고
    • Wilcox CD (1992) Turbulence modelling for CFD. DCW Industries, La Canada, California
  • 44
    • 0032025899 scopus 로고    scopus 로고
    • The effect of trailing edge geometry on cavity flow oscillation driven by a supersonic shear layer
    • Zhang X, Rona A, Edwards JA (1998) The effect of trailing edge geometry on cavity flow oscillation driven by a supersonic shear layer. Aero J 102:129-136
    • (1998) Aero J , vol.102 , pp. 129-136
    • Zhang, X.1    Rona, A.2    Edwards, J.A.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.