An experimental investigation on transpiration cooling under supersonic condition using a nose cone model-Reference-Cited by-同舟云学术

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An experimental investigation on transpiration cooling under supersonic condition using a nose cone model

Published:2014-10 Issue: Volume:84 Page:207-213
ISSN:1290-0729
Container-title:International Journal of Thermal Sciences
language:en
Short-container-title:International Journal of Thermal Sciences

Author:

Zhao Lianjin,Wang Jianhua,Ma Jie,Lin Jia,Peng Jinlong^ORCID,Qu Dejun,Chen Lianzhong

Publisher

Elsevier BV

Subject

General Engineering,Condensed Matter Physics

Reference21 articles.

1. High speed propulsion: performance advantage of advanced materials;Jackson;J. Mater. Sci.,2004

2. Transpiration cooling tests of porous CMC in hypersonic flow;Reimer,2011

3. Ceramic matrix composite (CMC) thermal protection systems (TPS) and hot structures for hypersonic vehicles;Glass,2008

4. Investigation of transpiration cooling effectiveness for air-breathing hypersonic vehicles;Gulli;AIAA Pap.,2011

5. A discussion of transpiration cooling problems through an analytical solution of local thermal nonequilibrium model;Wang;J. Heat Transfer Trans. ASME,2006

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4. Numerical simulation and structural optimization of transpiration cooling with gradient porous matrix in supersonic condition;International Journal of Thermal Sciences;2024-04

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