Maintenance of Operational Stability in Liquid-Propellant Rocket Engines by Adjusting the Acoustic Properties of the Combustion Chambers

S. V. Mosolov; V. I. Biryukov

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Maintenance of Operational Stability in Liquid-Propellant Rocket Engines by Adjusting the Acoustic Properties of the Combustion Chambers

机译：通过调节燃烧室的声学特性来维持液体火箭发动机的运行稳定性

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In liquid-propellant rocket engines, acoustic absorbers must be used to improve the stability of the combustion chambers with respect to some likely vibrational modes.

机译：在液体推进火箭发动机中，必须使用吸声器来改善燃烧室在某些可能的振动模式方面的稳定性。

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《Russian engineering research》 |2013年第6期|共6页
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S. V. Mosolov; V. I. Biryukov;
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1. Maintenance of Operational Stability in Liquid-Propellant Rocket Engines by Adjusting the Acoustic Properties of the Combustion Chambers [J] . S. V. Mosolov, V. I. Biryukov Russian engineering research . 2013,第6期

机译：通过调节燃烧室的声学特性来维持液体火箭发动机的运行稳定性
2. Mathematical Modeling and Experimental Investigations of Oxygen-Methane Fuel Combustion at Coaxial-Jet Supply into the Combustion Chamber of Liquid-Propellant Rocket Engine [J] . V. R. Rubinskii, S. P. Khrisanfov, V. Yu. Klimov, Russian Aeronautics . 2010,第1期

机译：液体推进火箭发动机同轴射流供氧-甲烷燃料燃烧的数学模型与实验研究
3. Damping Decrements in the Combustion Chambers of Liquid-Propellant Rocket Engines [J] . V. I. Biryukov, R. A. Tsarapkin Russian engineering research . 2019,第1期

机译：液体推进式火箭发动机的燃烧室中的阻尼递减
4. Low-Order Modelling of the Non-Local Acoustic Reacting Combustion Chamber-Dome Interface in Rocket Engines [C] . M. Schulze, T. Sattelmayer AIAA international space planes and hypersonic systems and technologies conference;AIAA aviation forum . 2014

机译：火箭发动机中非局部声反应燃烧室-圆顶接口的低阶建模
5. High-frequency combustion instability control through acoustic modulation at the inlet boundary for liquid rocket engine applications [D] . Bennewitz, John William 2015

机译：在液体火箭发动机应用中通过进气口处的声调制来进行高频燃烧不稳定性控制
6. Dataset of the experimentally measured heat transfer in the throat region of liquid rocket engine thrust chambers [O] . Marco Pizzarelli 2021

机译：实验测量的热传递的数据集在液体火箭发动机推力室的喉部区域中的热传递
7. Innovative methodology for calculation and design of liquid-propellant rocket engine combustion chamber [O] . О.В. Короткая 2016

机译：液相推进火箭发动机燃烧室计算与设计的创新方法
8. An Experimental Correlation of the Nonreactive Properties of Injection Schemes and Combustion Effects in a Liquid-Propellant Rocket Engine. Part 5 - on the Influence of Vanes on Combustion Stability [R] . Rupe, J. H. 1967

机译：液体火箭发动机喷射方案非反应特性与燃烧效应的实验关联。第5部分 - 关于叶片对燃烧稳定性的影响

Maintenance of Operational Stability in Liquid-Propellant Rocket Engines by Adjusting the Acoustic Properties of the Combustion Chambers

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