Numerical study of stratified charge combustion in wave rotors
Author:
Affiliation:
1. NASA, Lewis Research Center, Cleveland, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1997-3141
Reference34 articles.
1. and Power, vol.119.p. 469,April 1997; also
2. AIAA-95-2799,NASATM-106998.
3. Nalim, M. R. 'The Thermodynamic Limit of Pressure-Gain and Work-Producing Combustors", NASATechnicalMemo.,tobepublished, 1997.
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1. Mixing and Ignition Potential of Transient Confined Turbulent Jet in a Wave Rotor Combustor;46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2010-07-25
2. Two-Dimensional Flow and NOx Emissions in Deflagrative Internal Combustion Wave Rotor Configurations;Journal of Engineering for Gas Turbines and Power;2003-07-01
3. Assessment of Combustion Modes for Internal Combustion Wave Rotors;Journal of Engineering for Gas Turbines and Power;1999-04-01
4. Pulse combustion and wave rotors for high-speed propulsion engines;8th AIAA International Space Planes and Hypersonic Systems and Technologies Conference;1998-04-27
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