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On the design of acoustic liners for rocket engines - Helmholtz resonators evaluated with a rocket combustor

机译：关于火箭发动机声学衬垫的设计 - 用火箭燃烧器评估亥姆霍兹共振器

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Helmholtz resonators with variable cavity depths tested with unstable rocket combustor

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作者
Hannum, N. P.; Phillips, B.; Russell, L. M.;
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年度 1969
页码 1-28
总页数 28
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
CAVITY RESONATORS; COMBUSTION CHAMBERS; HELMHOLTZ VORTICITY EQUATION; ROCKET LININGS; ACOUSTIC PROPERTIES; APERTURES; GAS FLOW; GRAPHS (CHARTS); PARTIAL DIFFERENTIAL EQUATIONS; PRESSURE OSCILLATIONS;

机译：CaVITY REsONaTORs;燃烧室; HELmHOLTZ VORTICITY方程;火箭衬里;声学特性;小孔;气流;图表（图表）;部分微分方程;压力振荡;

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专利

1. Mapping the Influence of Acoustic Resonators on Rocket Engine Combustion Stability [J] . K. Foerner, A. Cardenas Miranda, W. Polifke Journal of propulsion and power . 2015,第4期

机译：绘制声谐振器对火箭发动机燃烧稳定性的影响
2. Establishment Of Design Method For Liquid Hydrogen Regenerative Cooling Combustor Of Lox/hydrogen Rocket Engine [J] . Nobuyuki Yatsuyanagi Transactions of the Japan society for aeronautical and space sciences . 2009,第174期

机译：Lox /氢火箭发动机液态氢蓄冷冷却器设计方法的建立
3. AIRCRAFT AND ROCKET ENGINE DESIGN AND DEVELOPMENT SIMULATION OF MIXING PROCESS GAS DYNAMICS IN THE GTE COMBUSTOR [J] . S. Yu. Kuznetsov V. F. Kharitonov, G. P. Grebenyuk Russian Aeronautics . 2003,第2期

机译：GTE燃烧室混合气体动力学的飞机火箭发动机设计与仿真。
4. Acoustic modification prediction using FRF: application of Helmholtz resonators on a rocket engine combustion chamber [C] . G. P. Guimaraes, R. Pirk, C. DA. Souto, International Conference on Noise and Vibration Engineering . 2012

机译：使用FRF的声学修改预测：Helmholtz谐振器在火箭发动机燃烧室中的应用
5. Computational investigations of high frequency acoustics and instabilities in a single-element rocket combustor. [D] . Smith, Randolph Jedediah. 2010

机译：单元件火箭燃烧室中高频声学和不稳定性的计算研究。
6. Ignition and Flame Stabilization of a Strut-Jet RBCC Combustor with Small Rocket Exhaust [O] . Jichao Hu, Juntao Chang, Wen Bao -1

机译：带有小火箭排气的Strutjet RBCC燃烧器的点火和火焰稳定
7. Development of Analysis Code for Evaluation of Acoustic Stability of Rocket Engine Combustor with Various Designs [O] . 2004

机译：具有各种设计的火箭发动机燃烧器声学稳定性评价分析码的开发
8. On the Design of Acoustic Liners for Rocket Engines - Helmholtz Resonators Evaluated with a Rocket Combustor [R] . Hannum, N. P., Phillips, B., Russell, L. M. 1969

机译：火箭发动机声学衬垫的设计 - 用火箭燃烧器评估亥姆霍兹谐振器

On the design of acoustic liners for rocket engines - Helmholtz resonators evaluated with a rocket combustor

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