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Cited article:
H. Riedmann, D. Banuti, B. Ivancic, O. Knab, K. Hannemann
Published online: 2019-02-08
This article has been cited by the following article(s):
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Energies 13 (24) 6616 (2020)
DOI: 10.3390/en13246616
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A detailed modelling on spray atomisation and combustion of LOX/GCH4 in variable area pintle injector rocket engines
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Multi-Phase Impact on the Heat Load Characteristics of a Multi-Element Methane-Oxygen Rocket Thrust Chamber
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International Journal of Heat and Mass Transfer 172 121113 (2021)
DOI: 10.1016/j.ijheatmasstransfer.2021.121113
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Special Cases of Using Visualization Technology for Analyzing the Dynamics of Gaseous Environment
Mikhail Sotskiy, Denis Levin and Victor Selivanov
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Timescale-Based Frozen Nonadiabatic Flamelet Combustion Modeling for Rocket Engine Thrust Chambers
Daniel Rahn, Oskar Haidn and Hendrik Riedmann
Journal of Propulsion and Power 37 (4) 495 (2021)
DOI: 10.2514/1.B37936
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