Coupled transpiration and film cooling characteristics of injector porous plate in a 45-element rocket thrust chamber

Aerospace Science and Technology 2026

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Authors: Cheng Xiong, Xin Wang, Mengmeng Cheng, Z. Andy Chen

DOI: 10.1016/j.ast.2026.111641

Cited by: 3

References: 33

Fields of Study & Subjects

Rocket and propulsion systems research Heat and Mass Transfer in Porous Media Combustion and flame dynamics

References 33