Abstract
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Tyler T. Evans, Alexander J. Smits
Abstract
Rights: UNKNOWN · https://www.elsevier.com/tdm/userlicense/1.0/ · Source: journal-auto-sync:external:CROSSREF_ISSN
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A Supersonic Turbulent Boundary Layer in an Adverse Pressure Gradient
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1988
The Response of a Compressible Turbulent Boundary Layer to Short Regions of Concave Surface Curvature
10.1017/s0022112087000429 · 1987
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1987
Three-Dimensional Separation for Interaction of Shock Waves and Turbulent Boundary Layers
10.2514/3.50634 · 1973
Detailed Study of Attached and Separated Compression Corner Flowfields in High Reynolds Number Supersonic Flow
10.2514/3.61180 · 1979
The Structure of Turbulence in a ShockWave/Boundary-Layer Interaction
10.2514/3.48565 · 1983
Turbulent Boundary Layer Properties Downstream of the Shock-Wave/Boundary-Layer Interaction
10.2514/3.9681 · 1986
Compilation of Wall Pressure Data for a Shock Wave-Turbulent Boundary Layer Interaction Generated by a Blunt Fin
1990
An Experimental Documentation of Supersonic Turbulent Flows in the Vicinity of Sloping Forward and Back Facing Steps
1990
Thin Film Heat Transfer Gage Construction and Measurement Details
1982
Experimental Study of 3 Shock Wave-Turbulent Boundary Layer Interactions
10.1017/s0022112087002349 · 1987
Use of Preston Tubes for Measuring Hypersonic Turbulent Skin Friction
1969
Reduction of Data from Thin-Film Heat Transfer Gages: A Concise Numerical Technique
10.2514/3.3486 · 1966
Heat Transfer Measurements in Short Duration Hypersonic Facilities
1973
Organized Structures in a Compressible Turbulent Boundary Layer
10.1017/s0022112087002258 · 1987
An Experimental Study of Compressible Turbulent Boundary Layer Separation at High Reynolds Numbers
1975
Model Instrumentation Techniques for Heat Transfer and Force Measurements in a Hypersonic Shock Tunnel
1956
The Near-Wall Temperature Profile of Turbulent Boundary Layers
1988
Three-Dimensional Flow Fields Generated by the Interaction of a Swept Shock Wave with a Turbulent Boundary Layer
1976
A Spectral Element Method for Fluid Dynamics: Laminar Flow in a Channel Expansion
10.1016/0021-9991(84)90128-1 · 1984
Unresolved referenced work
1989
A Preliminary Report on the Princeton University High Reynolds Number 8″ × 8″ Supersonic Tunnel
1971
Heat Transfer Measurement in a Turbulent Boundary Layer-Shock Wave Interaction
1992
Conventional Skin Friction Measurement Techniques for Strongly Perturbed Supersonic Turbulent Boundary Layers
1992
The Drag of a Compressible Turbulent Boundary Layer in a Smooth Flat Plate With and Without Heat Transfer
10.1017/s0022112064000088 · 1964
Summary of Available Information of Reynolds Analogy for Zero-Pressure-Gradient, Compressible, TurbulentBoundary-Layer Flow
1970
The Response of Turbulent Boundary Layers to Sudden Pertubations
10.1146/annurev.fl.17.010185.001541 · 1985
No additional external references are available.