Jet-A fuel evaporation analysis in conical tube injectors
Author:
Affiliation:
1. Wayne State University, Detroit, MI
2. NASA, Lewis Research Center, Cleveland, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1991-345
Reference50 articles.
1. A comparison of vaporization models in spray calculations
2. Aggarwal, S. K.andShuenJ.S.(1989) "Vaporization BehaviorofTurbulentPolydisperseand 'Equivalent' MonodisperseSprays,"J. Propulsion, V. 5(2),pp. 151-153. M e n , A. A., O'Rourke, P. J., andButler,T. D. (1989) "KIVA-II: AComputerProgramforChemicalReactive Flowswith Sprays," LosAlamosReportLA-11560-MS.
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1. Optimization of Swirler-Venturi Mixer Geometry for Fuel Reformer Application;3rd International Energy Conversion Engineering Conference;2005-06-19
2. Spray and Fuel-Air Mixing of the Swirler/Venturi Injectors for Lean Premixed Prevaporized Combustor;42nd AIAA Aerospace Sciences Meeting and Exhibit;2004-01-05
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