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High-frequency combustion instability control through acoustic modulation at the inlet boundary for liquid rocket engine applications

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

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作者
Bennewitz, John William;
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作者单位

The University of Alabama in Huntsville;

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授予单位 The University of Alabama in Huntsville;
学科
学位 Ph.D.
年度 2015
页码 262 p.
总页数 262
原文格式 PDF
正文语种 eng
中图分类
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专利

1. Combustion Instability Control Through Acoustic Modulation at the Inlet Boundary: Experiments [J] . John W. Bennewitz, Robert A. Frederick Jr., Jacob T. Cranford, Journal of propulsion and power . 2015,第6期

机译：通过入口边界处的声调制来控制燃烧不稳定性：实验
2. Combustion Instability Control Through Acoustic Modulation at the Inlet Boundary: Analysis [J] . John W. Bennewitz, Sarma L. Rani, Jacob T. Cranford, Journal of propulsion and power . 2015,第6期

机译：通过入口边界处的声调制控制燃烧不稳定性：分析
3. On the Method for Hot-Fire Modeling of High-Frequency Combustion Instability in Liquid Rocket Engines [J] . Chae Hoon Sohn, Woo-Seok Seol, Alexander A. Shibanov, KSME International Journal . 2004,第6期

机译：液体火箭发动机高频燃烧不稳定性热火建模方法研究
4. Application of Band-Limited White Noise Single Frequency Acoustic Modulation as a Control Mechanism for Liquid Rocket Engine Combustion Instabilities [C] . John W. Bennewitz, Jacob T. Cranford, David M. Lineberry, AIAA/ASME/SAE/ASEE joint propulsion conference;AIAA propulsion and energy forum . 2014

机译：带限白噪声和单频声学调制作为液体火箭发动机燃烧不稳定性控制机构的应用
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. 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. Nonlinear analysis of low-frequency combustion instabilities in liquid rocket engines [O] . M. Leonardi, F. Di Matteo, J. Steelant, 2019

机译：液体火箭发动机低频燃烧不稳定性的非线性分析
8. Solid Propellant Instability of Combustion 1964. Appendix I: Theory of Acoustic Instability in Solid Rocket Combustion. Appendix II: Experimental Solid Rocket Combustion Instability [R] . Hart, R. W., McClure, F. T., Price, E. W., 1964

机译：固体推进剂燃烧不稳定性1964.附录I：固体火箭燃烧中的声学不稳定性理论。附录II：实验固体火箭燃烧不稳定性

High-frequency combustion instability control through acoustic modulation at the inlet boundary for liquid rocket engine applications

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