Numerical study of acoustic resonance in a LOX injector post induced by orifice flow
Author:
Affiliation:
1. German Aerospace Center (DLR)
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2021-3568
Reference39 articles.
1. Liquid Rocket Engine Combustion Instability
2. Injector-Driven Combustion Instabilities in a Hydrogen/Oxygen Rocket Combustor
3. Injector-Driven Flame Dynamics in a High-Pressure Multi-Element Oxygen–Hydrogen Rocket Thrust Chamber
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. Orifice Flow Dynamics in a Rocket Injector as an Excitation Source of Injector-Driven Combustion Instabilities;Aerospace;2023-05-15
2. Impact of shear-coaxial injector hydrodynamics on high-frequency combustion instabilities in a representative cryogenic rocket engine;International Journal of Spray and Combustion Dynamics;2022-03
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