-
1
-
-
0000054178
-
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
-
-
Baldwin BS, Barth TJ (1990) A one-equation turbulence model for high Reynolds number wall bounded flows. NASA TM102847
-
-
-
-
3
-
-
84988040586
-
-
Baldwin BS, Lomax H (1978) Thin layer approximation and algebraic model for separated turbulent flows. AIAA78-257
-
-
-
-
4
-
-
84987935418
-
-
Boyce RR, Hillier R (2000) Shock-induced three-dimensional separation of an axisymmetric hypersonic turbulent boundary layer. AIAA 2000-2226
-
-
-
-
5
-
-
0023849835
-
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
-
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
-
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
-
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
-
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
-
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
-
12
-
-
84912262813
-
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
-
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
-
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
-
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
-
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
-
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
-
-
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
-
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
-
-
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
-
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
-
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
-
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
-
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
-
26
-
-
0034367061
-
Gun tunnel flow calibration: Defining input conditions for hypersonic flow computations
-
Mallinson SG, Hillier R, Jackson AP, Kirk DC, Soltani S, Zanchetta MA (2000) Gun tunnel flow calibration: defining input conditions for hypersonic flow computations. Shock Waves 10:313-322
-
(2000)
Shock Waves
, vol.10
, pp. 313-322
-
-
Mallinson, S.G.1
Hillier, R.2
Jackson, A.P.3
Kirk, D.C.4
Soltani, S.5
Zanchetta, M.A.6
-
27
-
-
0031356558
-
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
-
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
-
-
Oberkampf WL (2000) Design, execution and analysis of validation experiments. Verification and validation in CFD, VKI-lecture series
-
-
-
-
30
-
-
0029761838
-
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
-
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
-
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
-
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
-
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
-
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
-
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
-
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
-
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
-
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
-
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
-
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
-
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
-
-
Wilcox CD (1992) Turbulence modelling for CFD. DCW Industries, La Canada, California
-
-
-
-
44
-
-
0032025899
-
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
|