Fluorescent paint for measurement of heat transfer in shock - turbulent boundary layer interaction

Author:

Liu Tianshu,Campbell Bryan T.,Sullivan John P.

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Aerospace Engineering,Nuclear Energy and Engineering,General Chemical Engineering

Reference44 articles.

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

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