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Cited article:

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A new LES approach to trans-critical mixing and combustion processes in high-pressure liquid-injectant engines

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Flame characteristics of a high-pressure LOX/H2 rocket combustor with large optical access

Jan Martin, Wolfgang Armbruster, Robert Stützer, Stephan General, Bernhard Knapp, Dmitry Suslov and Justin Hardi
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Numerical study of the pseudo-boiling phenomenon in the transcritical liquid oxygen/gaseous hydrogen flame

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Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 235 (8) 893 (2021)
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Real Gas Models in Coupled Algorithms Numerical Recipes and Thermophysical Relations

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Numerical Simulation of a GH2/LOx Single Injector Combustor and the Effect of the Turbulent Schmidt Number

Won-Sub Hwang, Woojoo Han, Kang Y. Huh, Juhoon Kim, Bok Jik Lee and Jeong-Yeol Choi
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Explosion of Microbubbles Generated by the Alternating Polarity Water Electrolysis

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DESIGN AND ANALYSIS OF FIRST STAGE ROCKET ENGINE USING BUTANE AND LIQUID OXYGEN

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Real Gas Model Parameters for High-Density Combustion from Chemical Kinetic Model Data

Chenwei Zheng, Deshawn Murray Coombs and Benjamin Akih-Kumgeh
ACS Omega 4 (2) 3074 (2019)
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Numerical Simulation of Liquid Fuel Injection in Combustion Chamber

Syed Azeem Inam, Mukkarum Hussain and Mirza Mehmood Baig
Arabian Journal for Science and Engineering 44 (6) 5889 (2019)
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CFD simulations of turbulent nonreacting and reacting flows for rocket engine applications

Martin J. Seidl, Manfred Aigner, Roman Keller and Peter Gerlinger
The Journal of Supercritical Fluids 121 63 (2017)
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