Study of Cryogenic LOX/Kerosene Ignition and Flame Characteristics in a Single injector Combustion Chamber

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Eskandari, Mohammad Amin | 2014

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Type of Document: M.Sc. Thesis
Language: Farsi
Document No: 45787 (45)
University: Sharif University of Technology
Department: Aerospace Engineering
Advisor(s): Farshchi, Mohammad
Abstract:
This thesis discusses design and, simulation procedure of a mono-injector combustion chamber, in order to study and, analyze the ignition and, stable combustion characteristics, for Kerosene and, liquid Oxygen cryogenic propellants. Accordingly, the design and, simulation for the combustion chamber, for Kerosene and, liquid Oxygen propellants is performed. Also, effective parameters on the flame taking place are studied, and finally an algorithm for design and, properties study of cryogenic propellant ignition is presented
Keywords:
Combustion Chamber ; Design ; Reactor ; Simulation ; Cryogenic

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