Numerical Simulation of a GH<sub>2</sub>/LOx Single Injector Combustor and the Effect of the Turbulent Schmidt Number

Numerical Simulation of a GH<sub>2</sub>/LOx Single Injector Combustor and the Effect of the Turbulent Schmidt Number

A large-eddy simulation (LES) of a gaseous hydrogen/liquid oxygen (GH<sub>2</sub>/LO<sub>X</sub>) single-injector rocket combustor is performed in this study. The Redlich–Kwong–Peng–Robinson (RK–PR) equation of state is used to simulate the real-gas effect under high-pressure...

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Bibliographic Details
Main Authors: Won-Sub Hwang, Woojoo Han, Kang Y. Huh, Juhoon Kim, Bok Jik Lee, Jeong-Yeol Choi
Format: Article
Language:English
Published: MDPI AG 2020-12-01
Series:Energies
Subjects:
large-eddy simulation (LES)
RCM-3 combustor
Redlich–Kwong–Peng-Robinson equation of state
steady laminar flamelet model
turbulent Schmidt number
Online Access:https://www.mdpi.com/1996-1073/13/24/6616

Internet

https://www.mdpi.com/1996-1073/13/24/6616

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