Wall modeling of reacting turbulent flow and heat transfer in liquid rocket engines
Author:
Affiliation:
1. Japan Aerospace Exploration Agency (JAXA)
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-4870
Reference25 articles.
1. Hot-gas-side and coolant-side heat transfer in liquid rocket engine combustors
2. Validation of High-Fidelity CFD Simulations for Rocket Injector Design
3. Numerical Investigation of Flow and Combustion in a Single Element GCH4/Gox Rocket Combustor
4. Qualitative and Quantitative Comparison of RANS Simulation Results for a 7-Element GOX/GCH4 Rocket Combustor
Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Initial Investigations of Wall Models for Liquid Rocket Injector Simulations;AIAA Scitech 2021 Forum;2021-01-04
2. Simulation of the GOx/GCH4 Multi-Element Combustor Including the Effects of Radiation and Algebraic Variable Turbulent Prandtl Approaches;Energies;2020-09-23
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