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This article has been cited by the following article(s):
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Conceptual Design of a LOX/Methane Rocket Engine for a Small Launcher Upper StageCheulwoong Kim, Byoungjik Lim, Junseong Lee, et al.
Journal of the Korean Society of Propulsion Engineers 26 (4) 54 (2022)
An efficient modeling framework for wall heat flux prediction in rocket combustion chambers using non adiabatic flamelets and wall-functionsG. Indelicato, P.E. Lapenna, A. Remiddi and F. Creta
International Journal of Heat and Mass Transfer 169 120913 (2021)