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0023384745
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Some new aspects of the shock-wave/boundary-layer interaction in compression ramp flows
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0542368504
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Fluctuations and massive separation in three-dimensional shock wave/boundary layer interactions
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0024673746
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Separation shock motion in fin, cylinder, and compression ramp induced turbulent interactions
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0012445040
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Dynamics of separation and reattachment in a mach 5 unswept compression ramp flow
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AIAA Paper 90-0380, Jan
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Gramann, R.A.1
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5
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Detection of turbulent boundary-layer separation using fluctuating wall pressure signals
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Unsteady wave structure near separation in a mach 5 compression ramp interaction
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Effect of periodic blowing on attached and separated supersonic turbulent boundary layers
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Correlation of separation shock motion with pressure fluctuations in the incoming boundary layer
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An experimental study of the driving mechanism and control of the unsteady shock induced turbulent separation in a mach 5 compression corner flow
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Ph.D. Dissertation, Dept. of Aerospace Engineering and Engineering Mechanics, Univ. of Texas, Austin, TX, Aug
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10
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Computation of turbulent, separated, unswept compression ramp interactions
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0003677645
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Fluctuating loads in shock wave/turbulent boundary layer interaction: Tutorial and update
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AIAA Paper 93-0284, Jan
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Physical causes of separation shock unsteadiness in shock wave/turbulent boundary layer interactions
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AIAA Paper 93-3134, July
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Erengil, M. E., and Dolling, D. S., "Physical Causes of Separation Shock Unsteadiness in Shock Wave/Turbulent Boundary Layer Interactions," AIAA Paper 93-3134, July 1993.
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Physics of unsteady blunt-fin-induced shock wave/turbulent boundary layer interactions
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Decay of wall pressure field and structure of a mach 5 adiabatic turbulent boundary layer
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AIAA Paper 94-2363, June
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Planar laser scattering imaging of shock wave turbulent boundary layer interactions
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M.S. Thesis, Dept. of Aerospace Engineering and Engineering Mechanics, Univ. of Texas, Austin, TX, Nov
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Chan, S.C.1
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16
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0012381418
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Investigation of the causes of large-scale unsteadiness of shock-induced separated flow using planar laser imaging
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AIAA Paper 97-0064, Jan
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Beresh, S. J., Clemens, N. T., Dolling, D. S., and Comninos, M., "Investigation of the Causes of Large-Scale Unsteadiness of Shock-Induced Separated Flow Using Planar Laser Imaging," AIAA Paper 97-0064, Jan. 1997.
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The effects of the incoming turbulent boundary layer structure on a shock-induced separated flow
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AIAA Paper 98-0629, Jan
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Beresh, S. J., Comninos, M., Clemens, N. T., and Dolling, D. S., "The Effects of the Incoming Turbulent Boundary Layer Structure on a Shock-Induced Separated Flow," AIAA Paper 98-0629, Jan. 1998.
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Beresh, S.J.1
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0003994663
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A very large-eddy simulation of an unsteady shock wave/turbulent boundary layer interaction
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AIAA Paper 95-2212, June
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Hunt, D.1
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0033197440
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Decay of fluctuating wall-pressure field of a mach 5 turbulent boundary layer
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Ünalmis, O. H., and Dolling, D. S., "Decay of Fluctuating Wall-Pressure Field of a Mach 5 Turbulent Boundary Layer," AIAA Journal, Vol. 37, No. 9, 1999, pp. 1088-1096.
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The effect of the incoming turbulent boundary layer on a shock-induced separated flow using particle image velocimetry
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Ph.D. Dissertation, Dept. of Aerospace Engineering and Engineering Mechanics, Univ. of Texas, Austin, TX, Aug
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0012478717
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Using particle image velocimetry in difficult facilities: Some lessons learned
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Experimental study of causes of unsteadiness of shock-induced turbulent separation
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0012387771
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A preliminary study of turbulent structures associated with unsteady separation shock motion in a mach 5 compression ramp interaction
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AIAA Paper 92-0744, Jan
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The effect of a discrete window offset on the accuracy of cross-correlation analysis of digital PIV recordings
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Investigation into the cause of unsteadiness of shock wave/turbulent boundary layer interaction using planar laser scattering
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M.S. Thesis, Dept. of Aerospace Engineering and Engineering Mechanics, Univ. of Texas, Austin, TX, Dec
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Comninos, M., "Investigation into the Cause of Unsteadiness of Shock Wave/Turbulent Boundary Layer Interaction using Planar Laser Scattering," M.S. Thesis, Dept. of Aerospace Engineering and Engineering Mechanics, Univ. of Texas, Austin, TX, Dec. 1997.
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The relationship between upstream turbulent boundary layer velocity fluctuations and separation shock unsteadiness
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