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1
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0025387940
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A Supersonic Turbulent Boundary Layer in an Adverse Pressure Gradient
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Fernando, E. M., and Smits, A. J., A Supersonic Turbulent Boundary Layer in an Adverse Pressure Gradient, J. Fluid Mech. 211, 285-302, 1988.
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(1988)
J. Fluid Mech.
, vol.211
, pp. 285-302
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Fernando, E.M.1
Smits, A.J.2
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2
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85007141152
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Supersonic Turbulent Boundary Layers with Strong Adverse and Favorable Pressure Gradients
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Buffalo, NY
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Smith, D. R., and Smits, A. J., Supersonic Turbulent Boundary Layers with Strong Adverse and Favorable Pressure Gradients, Paper FE7, 41st APS Fluid Dynamics Meeting, Buffalo, NY, 1988.
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(1988)
Paper FE7, 41st APS Fluid Dynamics Meeting
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Smith, D.R.1
Smits, A.J.2
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3
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0023288466
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The Response of a Compressible Turbulent Boundary Layer to Short Regions of Concave Surface Curvature
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Jayaram, M., Taylor, M. W., and Smits, A. J., The Response of a Compressible Turbulent Boundary Layer to Short Regions of Concave Surface Curvature, J. Fluid Mech. 175, 343-362, 1987.
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(1987)
J. Fluid Mech.
, vol.175
, pp. 343-362
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Jayaram, M.1
Taylor, M.W.2
Smits, A.J.3
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4
-
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84971730703
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A Preliminary Investigation of Large-Scale Organized Motions in a Supersonic Turbulent Boundary Layer on a Concave Surface
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Donovan, J. F., and Smits, A. J., A Preliminary Investigation of Large-Scale Organized Motions in a Supersonic Turbulent Boundary Layer on a Concave Surface, AIAA Paper 87-1285, 1987.
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(1987)
AIAA Paper 87-1285
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Donovan, J.F.1
Smits, A.J.2
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5
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0015680606
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Three-Dimensional Separation for Interaction of Shock Waves and Turbulent Boundary Layers
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Goldberg, T. J., Three-Dimensional Separation for Interaction of Shock Waves and Turbulent Boundary Layers, AIAA J. 11, 1573-1579, 1973.
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AIAA J.
, vol.11
, pp. 1573-1579
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Goldberg, T.J.1
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6
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0018479027
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Detailed Study of Attached and Separated Compression Corner Flowfields in High Reynolds Number Supersonic Flow
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Settles, G. S., Fitzpatrick, T. J., and Bogdonoff, S. M., Detailed Study of Attached and Separated Compression Corner Flowfields in High Reynolds Number Supersonic Flow, AIAA J. 17, 579-585, 1979.
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AIAA J.
, vol.17
, pp. 579-585
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Settles, G.S.1
Fitzpatrick, T.J.2
Bogdonoff, S.M.3
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7
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0021500870
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The Structure of Turbulence in a Shock-Wave/Boundary-Layer Interaction
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Ardonceau, P. L., The Structure of Turbulence in a Shock-Wave/Boundary-Layer Interaction, AIAA J. 22(9), 1254-1262, 1983.
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AIAA J.
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Ardonceau, P.L.1
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8
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0023341682
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Turbulent Boundary Layer Properties Downstream of the Shock-Wave/ Boundary-Layer Interaction
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Kuntz, D. W., Amatucci, V. A., and Addy, A. J., Turbulent Boundary Layer Properties Downstream of the Shock-Wave/ Boundary-Layer Interaction, AIAA J. 25(5), 668-675, 1986.
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AIAA J.
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Kuntz, D.W.1
Amatucci, V.A.2
Addy, A.J.3
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9
-
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3242869582
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Compilation of Wall Pressure Data for a Shock Wave-Turbulent Boundary Layer Interaction Generated by a Blunt Fin
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Evans, T. T., Poddar, K., and Smits, A. J., Compilation of Wall Pressure Data for a Shock Wave-Turbulent Boundary Layer Interaction Generated by a Blunt Fin, Princeton Univ. MAE Rep. 1908-T, 1990.
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(1990)
Princeton Univ. MAE Rep. 1908-T
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Evans, T.T.1
Poddar, K.2
Smits, A.J.3
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10
-
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0013449428
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An Experimental Documentation of Supersonic Turbulent Flows in the Vicinity of Sloping Forward and Back Facing Steps
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ITPM Rep. 2013, April
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Zheltovodov, A. A., Trofimov, V. M., Shilein, E. H., and Yakovlev, V. N., An Experimental Documentation of Supersonic Turbulent Flows in the Vicinity of Sloping Forward and Back Facing Steps, Inst. Theoretical and Applied Mechanics Siberia Div. of USSR Acad. Sci., ITPM Rep. 2013, April 1990.
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(1990)
Inst. Theoretical and Applied Mechanics Siberia Div. of USSR Acad. Sci.
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Zheltovodov, A.A.1
Trofimov, V.M.2
Shilein, E.H.3
Yakovlev, V.N.4
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11
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0342939199
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Thin Film Heat Transfer Gage Construction and Measurement Details
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March
-
Ligrani, P. M., Camci, C., and Grady, M. S., Thin Film Heat Transfer Gage Construction and Measurement Details, Von Kármán Institute for Fluid Dynamics Internal Note 72, March 1982.
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(1982)
Von Kármán Institute for Fluid Dynamics Internal Note
, vol.72
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Ligrani, P.M.1
Camci, C.2
Grady, M.S.3
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12
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0023410218
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Experimental Study of 3 Shock Wave-Turbulent Boundary Layer Interactions
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Smits, A. J., and Muck, K. C., Experimental Study of 3 Shock Wave-Turbulent Boundary Layer Interactions, J. Fluid Mech. 182, 291-314, 1987.
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(1987)
J. Fluid Mech.
, vol.182
, pp. 291-314
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Smits, A.J.1
Muck, K.C.2
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13
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0042362617
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Use of Preston Tubes for Measuring Hypersonic Turbulent Skin Friction
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TN D-5544, November
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Keener, E. R., and Hopkins, E. J., Use of Preston Tubes for Measuring Hypersonic Turbulent Skin Friction, NASA Tech. Note, TN D-5544, November 1969.
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(1969)
NASA Tech. Note
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Keener, E.R.1
Hopkins, E.J.2
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14
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85007670845
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Reduction of Data from Thin-Film Heat Transfer Gages: A Concise Numerical Technique
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Cook, W. J., and Felderman, E. J., Reduction of Data from Thin-Film Heat Transfer Gages: A Concise Numerical Technique, AIAA J. 4(3), 561-562, 1966.
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, Issue.3
, pp. 561-562
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Cook, W.J.1
Felderman, E.J.2
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15
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84865639176
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Heat Transfer Measurements in Short Duration Hypersonic Facilities
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Schultz, D. J., and Jones, T. V., Heat Transfer Measurements in Short Duration Hypersonic Facilities, AGARDograph 165, 1973.
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(1973)
AGARDograph
, pp. 165
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Schultz, D.J.1
Jones, T.V.2
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16
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0023147922
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Organized Structures in a Compressible Turbulent Boundary Layer
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Spina, E. F., and Smits, A. J., Organized Structures in a Compressible Turbulent Boundary Layer, J. Fluid Mech. 182, 85-109, 1987.
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(1987)
J. Fluid Mech.
, vol.182
, pp. 85-109
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Spina, E.F.1
Smits, A.J.2
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18
-
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0006693133
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Instrumentation Techniques for Heat Transfer and Force Measurements in a Hypersonic Shock Tunnel
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Vidal, R. J., Model Instrumentation Techniques for Heat Transfer and Force Measurements in a Hypersonic Shock Tunnel, Cornell Aeronautical Lab. Rep. AD-917-A-1, February 1956.
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(1956)
Cornell Aeronautical Lab. Rep. AD-917-A-1, February
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Vidal, R.J.1
Model2
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19
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4043127207
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The Near-Wall Temperature Profile of Turbulent Boundary Layers
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Carvin, D., Debiève, J. F., and Smits, A. J., The Near-Wall Temperature Profile of Turbulent Boundary Layers, AIAA Paper 88-0136, 1988.
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(1988)
AIAA Paper
, pp. 88-0136
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Carvin, D.1
Debiève, J.F.2
Smits, A.J.3
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21
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48549109395
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A Spectral Element Method for Fluid Dynamics: Laminar Flow in a Channel Expansion
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Patera, A., A Spectral Element Method for Fluid Dynamics: Laminar Flow in a Channel Expansion, J. Comput. Phys. 54, 466-468, 1984.
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, pp. 466-468
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Patera, A.1
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22
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0003474751
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Cambridge Univ. Press, UK
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Press, W. J., Flannery, B. P., Teukolsky, S. A., and Vetterling, W. T., Numerical Recipes: The Art of Scientific Computing, Cambridge Univ. Press, UK, 1989.
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(1989)
Numerical Recipes: the Art of Scientific Computing
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Press, W.J.1
Flannery, B.P.2
Teukolsky, S.A.3
Vetterling, W.T.4
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23
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85030012640
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A Preliminary Report on the Princeton University High Reynolds Number 8″ × 8″ Supersonic Tunnel
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Vas, I. E., and Bogdonoff, S. M., A Preliminary Report on the Princeton University High Reynolds Number 8″ × 8″ Supersonic Tunnel, Princeton Univ. Gas Dynamics Lab. Internal Rep. 39, 1971.
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Princeton Univ. Gas Dynamics Lab. Internal Rep. 39
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Vas, I.E.1
Bogdonoff, S.M.2
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25
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0026971318
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Conventional Skin Friction Measurement Techniques for Strongly Perturbed Supersonic Turbulent Boundary Layers
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Smith, D. R., Fernando, E. M., Donovan, J. F., and Smits, A. J., Conventional Skin Friction Measurement Techniques for Strongly Perturbed Supersonic Turbulent Boundary Layers, Eur. J. Mech. B 11(6), 719-740, 1992.
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(1992)
Eur. J. Mech. b
, vol.11
, Issue.6
, pp. 719-740
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Smith, D.R.1
Fernando, E.M.2
Donovan, J.F.3
Smits, A.J.4
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26
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84958438982
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The Drag of a Compressible Turbulent Boundary Layer in a Smooth Flat Plate with and Without Heat Transfer
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Spalding, D. B., and Chi, S. W., The Drag of a Compressible Turbulent Boundary Layer in a Smooth Flat Plate With and Without Heat Transfer, J. Fluid Mech. 18(1), 117-143, 1964.
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J. Fluid Mech.
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, Issue.1
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Spalding, D.B.1
Chi, S.W.2
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27
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0042362614
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Summary of Available Information of Reynolds Analogy for Zero-Pressure-Gradient, Compressible, Turbulent-Boundary-Layer Flow
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January
-
Cary, A. M., Jr., Summary of Available Information of Reynolds Analogy for Zero-Pressure-Gradient, Compressible, Turbulent-Boundary-Layer Flow, NASA Tech. Note, TN D-5560, January, 1970.
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NASA Tech. Note, TN D-5560
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Cary A.M., Jr.1
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28
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0021860473
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The Response of Turbulent Boundary Layers to Sudden Pertubations
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Smits, A. J., and Wood, D. W., The Response of Turbulent Boundary Layers to Sudden Pertubations, Annu. Rev. Fluid Mech. 17, 321-358, 1985.
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(1985)
Annu. Rev. Fluid Mech.
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Smits, A.J.1
Wood, D.W.2
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