1. Heat Transfer and Skin-Friction Measurements at a Mach Number of 2.44 for a Turbulent Boundary Layer on a Flat Surface in Regions of Separated Flows;Gadd;ARC R & M 3148,1958
2. An Investigation of Separated Flows. Part 2: Flow in the Cavity and Heat Transfer;Charwat;J. Aerosp. Sci.,1961
3. Heat Transfer Measurements and CFD Comparison of Swept Shock/Boundary-Layer Interactions;Lee;AIAA Paper 92-3665,1992
4. Experimental/Computational Studies of Sharp Fin Induced Shock Wave/Turbulent Boundary Layer Interactions at Mach 5: Experimental Results;Rodi;AIAA Paper 92-0749,1990
5. Fluctuation of Heat Transfer in Shock Wave/Turbulent Boundary Layer Interaction;Hayashi;AIAA J.,1989