Investigation of the open loop performance of an active control system utilizing a fuel injector actuator-Reference-Cited by-同舟云学术

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Investigation of the open loop performance of an active control system utilizing a fuel injector actuator

Published:1996-07-01 Issue: Volume: Page:
ISSN:
Container-title:32nd Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

Neumeier Yedidia¹,Nabi Aharon¹,Zinn Ben¹,Lewis, Jr. David¹

Affiliation:

1. Georgia Inst. of Technology, Atlanta

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1996-2757

Reference21 articles.

1. Harjee, D. and Reardon, F. (Eds.), "Liquid Propellant Rocket Combustion Instability", NASA SP 194,1972.

2. A review of active control of combustion instabilities

Cited by 5 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. The Model of Combustion Instability;Internal Combustion Processes of Liquid Rocket Engines;2016-05-20

2. Investigation of Combustion Control in a Dump Combustor Using the Feedback Free Fluidic Oscillator;51st AIAA/SAE/ASEE Joint Propulsion Conference;2015-07-23

3. ACTIVE INSTABILITY CONTROL EFFECTIVENESS IN A LIQUID FUELED COMBUSTOR;Combustion Science and Technology;2006-09

4. Nonlinear Modeling and Control of Combustion Dynamics;Control of Fluid Flow;2006

5. Sub-Scale Demonstration of the Active Feedback Control of Gas-Turbine Combustion Instabilities;Journal of Engineering for Gas Turbines and Power;2000-01-03

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