Research graph
References from Measurements of the mean heat transfer in a shock wave-turbulent boundary layer interaction. Local targets link to admitted publications; unresolved targets remain external evidence.
A Supersonic Turbulent Boundary Layer in an Adverse Pressure Gradient
10.1017/s0022112090001574 · 1988 · External reference
Supersonic Turbulent Boundary Layers with Strong Adverse and Favorable Pressure Gradients
1988 · External reference
The Response of a Compressible Turbulent Boundary Layer to Short Regions of Concave Surface Curvature
10.1017/s0022112087000429 · 1987 · External reference
A Preliminary Investigation of Large-Scale Organized Motions in a Supersonic Turbulent Boundary Layer on a Concave Surface
1987 · External reference
Three-Dimensional Separation for Interaction of Shock Waves and Turbulent Boundary Layers
10.2514/3.50634 · 1973 · External reference
Detailed Study of Attached and Separated Compression Corner Flowfields in High Reynolds Number Supersonic Flow
10.2514/3.61180 · 1979 · External reference
The Structure of Turbulence in a ShockWave/Boundary-Layer Interaction
10.2514/3.48565 · 1983 · External reference
Turbulent Boundary Layer Properties Downstream of the Shock-Wave/Boundary-Layer Interaction
10.2514/3.9681 · 1986 · External reference
Compilation of Wall Pressure Data for a Shock Wave-Turbulent Boundary Layer Interaction Generated by a Blunt Fin
1990 · External reference
An Experimental Documentation of Supersonic Turbulent Flows in the Vicinity of Sloping Forward and Back Facing Steps
1990 · External reference
Thin Film Heat Transfer Gage Construction and Measurement Details
1982 · External reference
Experimental Study of 3 Shock Wave-Turbulent Boundary Layer Interactions
10.1017/s0022112087002349 · 1987 · External reference
Use of Preston Tubes for Measuring Hypersonic Turbulent Skin Friction
1969 · External reference
Reduction of Data from Thin-Film Heat Transfer Gages: A Concise Numerical Technique
10.2514/3.3486 · 1966 · External reference
Heat Transfer Measurements in Short Duration Hypersonic Facilities
1973 · External reference
Organized Structures in a Compressible Turbulent Boundary Layer
10.1017/s0022112087002258 · 1987 · External reference
An Experimental Study of Compressible Turbulent Boundary Layer Separation at High Reynolds Numbers
1975 · External reference
Model Instrumentation Techniques for Heat Transfer and Force Measurements in a Hypersonic Shock Tunnel
1956 · External reference
The Near-Wall Temperature Profile of Turbulent Boundary Layers
1988 · External reference
Three-Dimensional Flow Fields Generated by the Interaction of a Swept Shock Wave with a Turbulent Boundary Layer
1976 · External reference
A Spectral Element Method for Fluid Dynamics: Laminar Flow in a Channel Expansion
10.1016/0021-9991(84)90128-1 · 1984 · External reference
Unresolved reference
1989 · External reference
A Preliminary Report on the Princeton University High Reynolds Number 8″ × 8″ Supersonic Tunnel
1971 · External reference
Heat Transfer Measurement in a Turbulent Boundary Layer-Shock Wave Interaction
1992 · External reference
Conventional Skin Friction Measurement Techniques for Strongly Perturbed Supersonic Turbulent Boundary Layers
1992 · External reference
The Drag of a Compressible Turbulent Boundary Layer in a Smooth Flat Plate With and Without Heat Transfer
10.1017/s0022112064000088 · 1964 · External reference
Summary of Available Information of Reynolds Analogy for Zero-Pressure-Gradient, Compressible, TurbulentBoundary-Layer Flow
1970 · External reference
The Response of Turbulent Boundary Layers to Sudden Pertubations
10.1146/annurev.fl.17.010185.001541 · 1985 · External reference
