Experimental investigation on transpiration cooling of ammonium carbonate in porous composite structure at high-temperature

Author:

Wang Fei,Song Nianduo,Xia Xinlin,Chen Xue

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Reference28 articles.

1. Injector head transpiration cooling coupled with combustion in H2/O2 subscale thrust chamber;Zhu;J. Thermophys. Heat Transfer,2013

2. Investigation of a porous transpiration-cooled strut injector;Huang;J. Propul. Power,2015

3. Investigation of inclined porous transpiration-cooled struts;Huang;J. Spacecr. Rocket.,2018

4. D. Greuel, A. Herbertz, O.J. Haidn, M. Ortelt, H. Hald, Transpiration Cooling Applied to C/C Liners of Cryogenic Liquid Rocket Engines, in: 40th AIAA/ASME/SAE/ASEE/JPC Conference and Exhibition, Fort Lauderdale, Florida, USA, 11.-14.07.2004, 2004.

5. Effusion cooled CMC rocket combustion chamber;Hald,2013

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