Numerical investigation of an active TPS for a wing leading edge exposed to high temperature air behind a strong bow shock wave

Author:

Ohwada Taku,Shimada Tomonori,Kato Takuma

Funder

The Kyoto University Foundation

Publisher

Springer Science and Business Media LLC

Reference10 articles.

1. Stalder JR, Inoue M (1956) A method of reducing heat transfer to blunt bodies. NACA RM A56B27a

2. Royal Aircraft Establishment, Farnborought, Hants;CHE Warren,1959

3. Swenson BL (1961) An approximate analysis of film cooling on blunt bodies by gas injection near the stagnation point. NASA TN D-861

4. Dannenberg RE (1962) Helium film cooling on a hemisphere at a Mach number of 10. NASA TN D-1550

5. Finley PJ (1966) The flow of a jet from a body opposing a supersonic free stream. J Fluid Mec 26:337–368

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