Relation of CARS temperature fields to lean blowout performance in an aircraft gas turbine generic combustor
- 27 June 1994
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 14 references indexed in Scilit:
- Modeling of Local Extinction in Turbulent FlamesPublished by ASME International ,1994
- Observations of Flame Behavior From a Practical Fuel Injector Using Gaseous Fuel in a Technology CombustorPublished by ASME International ,1994
- Modification of Combustor Stoichiometry Distribution for Reduced NOx Emission From Aircraft EnginesJournal of Engineering for Gas Turbines and Power, 1993
- Effects of Back-Pressure in a Lean Blowout Research CombustorJournal of Engineering for Gas Turbines and Power, 1993
- Isothermal Flow Fields in a Research Combustor for Lean Blowout StudiesJournal of Engineering for Gas Turbines and Power, 1992
- Design and Development of a Research Combustor for Lean Blow-Out StudiesJournal of Engineering for Gas Turbines and Power, 1992
- Acoustic characteristics of a research step combustorPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- BOXCARS: Crossed-beam phase-matched CARS generation in gasesApplied Physics Letters, 1978
- Modeling of Gas Turbine Combustors—A Convenient Reaction Rate EquationJournal of Engineering for Power, 1972
- The flame stability and heat release rates of some can-type combustion chambersSymposium (International) on Combustion, 1961