Numerical Investigation of Combustion of Cryogenic H2-O2 Propellant under Sub-Critical Condition, M.Sc. Thesis Sharif University of Technology ; Mardani, Amir (Supervisor) ; Farshchi, Mohammad (Supervisor)
Abstract
The present work is concerned with numerical simulation of spray flame for rocket combustor (MASCOTTE A-10 test case at 10 bar pressure) based on cryogen gaseous hydrogen and liquid oxygen at specific condition. This liquid oxygen and gaseous hydrogen single element combustor experiment has been the focus of many numerical studies which is representative of combustion in rocket combustion chamber condition. The purposed strategy relies on hybrid Eulerian-Lagrangian framework that continuous phase is evaluated by Reynolds average Navier-stokes (RANS) equation with quick discretization method and dispersed phase of combustion chamber atmosphere is evaluated by discrete phase method (DPM). To...
Cataloging briefNumerical Investigation of Combustion of Cryogenic H2-O2 Propellant under Sub-Critical Condition, M.Sc. Thesis Sharif University of Technology ; Mardani, Amir (Supervisor) ; Farshchi, Mohammad (Supervisor)
Abstract
The present work is concerned with numerical simulation of spray flame for rocket combustor (MASCOTTE A-10 test case at 10 bar pressure) based on cryogen gaseous hydrogen and liquid oxygen at specific condition. This liquid oxygen and gaseous hydrogen single element combustor experiment has been the focus of many numerical studies which is representative of combustion in rocket combustion chamber condition. The purposed strategy relies on hybrid Eulerian-Lagrangian framework that continuous phase is evaluated by Reynolds average Navier-stokes (RANS) equation with quick discretization method and dispersed phase of combustion chamber atmosphere is evaluated by discrete phase method (DPM). To...
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