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This article has been cited by the following article(s):
Effects of injector geometry on the combustion characteristics and stability of nonpremixed O2/CH4 coaxial flames in a model combustor
Young Hoo Kim, Tae Won Kim, Ju Han Kim, Hyeon Woo Lee, Jae Hyun Kim and Oh Chae Kwon Aerospace Science and Technology 162 110205 (2025) https://doi.org/10.1016/j.ast.2025.110205
Transonic Flow Field Analysis of a Minimum Nozzle Length Rocket Engine