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Theoretical, Numerical, and Experimental Investigations of the Fundamental Processes That Drive Combustion Instabilities in Liquid Rocket Engines.

机译：驱动液体火箭发动机燃烧不稳定性的基本过程的理论，数值和实验研究。

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The objective of this research was to develop an integrated theoretical and computational framework for treating combustion dynamics of cryogenic and hydrocarbon propellants under conditions representative of contemporary liquid rocket engines.

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作者
Quinlan, M.; Kim, Y. J.; Baroncelli, M.; Dumitrache, C.; Huo, H.;
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年度 2012
页码 1-12
总页数 12
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Liquid propellant rocket engines; Simulators; Acoustics; Combustion stability; Computation science; Fuel injectors; Laboratory equipment; Symposia; Briefing charts; Lre(Liquid rocket engine); Aclres(Actively controlled lre simulator); Supercritical combustion; Swirl injectors; Acoustic flame interaction; High fidelity modeling; Multiphase flow dynamics; Acoustic models;

机译：液体推进剂火箭发动机;模拟器;声学;燃烧稳定性;计算科学;燃料喷射器;实验室设备;专题讨论会;简报图; Lre（液体火箭发动机）; aclres（主动控制的模拟器）;超临界燃烧;旋流喷射器;声学火焰相互作用;高保真度建模;多相流动力学;声学模型;

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专利

1. Experimental investigation of high-frequency combustion instabilities in liquid rocket engine [J] . F. Richecoeur, S. Ducruix, P. Scouflaire, Acta astronautica . 2008,第1期

机译：液体火箭发动机高频燃烧不稳定性的实验研究
2. Experimental and numerical investigation of thermo-acoustic instability in a liquid-fuel aero-engine combustor at elevated pressure: Validity of large-eddy simulation of spray combustion [J] . Tachibana Shigeru, Saito Kinya, Yamamoto Takeshi, Combustion and Flame . 2015,第6期

机译：液体燃料航空发动机燃烧室在高压下热声不稳定性的实验和数值研究：喷雾燃烧大涡模拟的有效性
3. 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
4. Numerical Investigation on Combustion Instability in a small MMH/NTO Liquid Rocket Engine [C] . Jianxiu Qin, Huiqiang Zhang, Bing Wang AIAA/SAE/ASEE joint propulsion conference;AIAA propulsion and energy forum . 2016

机译：小型MMH / NTO液体火箭发动机燃烧不稳定性的数值研究
5. Computational fluid dynamic analyses of combustion instabilities in liquid rocket engines. [D] . Grenda, Jeffrey Michael. 1995

机译：液体火箭发动机燃烧不稳定性的计算流体动力学分析。
6. Experimental and numerical studies on combustion characteristics of N2-diluted CH4 and O2 diffusion combustion in a packed bed [O] . Houping Li, Junrui Shi, Mingming Mao, 2019

机译：填充床中N2稀释的CH4和O2扩散燃烧燃烧特性的实验和数值研究
7. Numerical Investigation of Combustion Instabilities in a Rocket Combustion Chamber with Supercritical Injection Using a Hybrid RANS/LES Method [O] . Ansgar Lechtenberg, Peter M. Gerlinger 2020

机译：用杂交rans / les法使用超临界注射液中火箭燃烧室燃烧不含的数值研究

Theoretical, Numerical, and Experimental Investigations of the Fundamental Processes That Drive Combustion Instabilities in Liquid Rocket Engines.

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