Control of combustion instabilities and emissions using an internally mixed liquid atomizer with a vaporizer
Author:
Affiliation:
1. Georgia Inst. of Technology, Atlanta
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2002-617
Reference24 articles.
1. Effects of Periodic Atomization on Combustion Instability in Liquid-Fueled Propulsion Systems
2. Mechanism of Combustion Instability in a Lean Premixed Dump Combustor
3. Investigation of oscillatory combustion processes in actively controlled liquid fuel combustor
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1. Controlled atomization using a twin-fluid swirl atomizer;Experiments in Fluids;2006-08-22
2. "Slow" Control of Combustion Instabilities by Fuel Spray Modification Using Smart Fuel Injector;42nd AIAA Aerospace Sciences Meeting and Exhibit;2004-01-05
3. Active Control of Instabilities in High-Pressure Combustor by Non-Coherent Oscillatory Fuel Injection;39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2003-06-26
4. Suppression of Combustion Instability by Controlling the Atomizing Properties in Liquid-Fueled Combustor;41st Aerospace Sciences Meeting and Exhibit;2003-01-06
5. The Dependence of Combustion Instability upon Liquid Fuel Spray Properties;38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2002-07-07
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