Research on thermal protection mechanism of forward-facing cavity and opposing jet combinatorial thermal protection system

Author:

Lu Hai-Bo,Liu Wei-Qiang

Publisher

Springer Science and Business Media LLC

Subject

Fluid Flow and Transfer Processes,Condensed Matter Physics

Reference25 articles.

1. Zhang F, Liu WQ (2007) Analysis of thermal wrinkling resulted from non-uniform temperature distribution in transpiration cooling formed platelets. Acta Aeronaut et Astronaut Sinica 28(1):138 (in Chinese)

2. Ye H, Geng X (2011) The feasibility analysis of the application of TPV system in reentry. Sci China Tech Sci 41(1):102 (in Chinese)

3. Glass DE (2006) Heat-pipe-cooled leading edges for hypersonic vehicles. NASA Langley Research Center July 12–13

4. Hartmann J, Troll B (1922) On a new method for the generation of sound waves. Phys Rev 20(6):719

5. Engblom WA, Goldstein DB (1997) Fluid dynamics of hypersonic forward-facing cavity flow. J Spacecr Rocket 34(4):437

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