Towards a Numerical Simulation of Supersonic Mixing & Combustion: Development & Validation of a Computational Solver for Two-Dimensional Compressible ... Perspectives on Reaching "A Certain Age" - Softcover
Synopsis
The design and off-design studies of the hypersonic air-breathing engines face many challenges, due to the complexity of their internal flows. The mixing and combustion processes in Supersonic-Combustion Ramjet (scramjet) engines involve complicated aerothermochemical features, such as: the interactions between shock-waves and boundary-layer, the shock induced-combustion and the recirculation zones. In this study, a numerical solver is developed and validated to be an efficient design tool capable of simulating these complicated flow features of the supersonic combustors. For the code validation, several test cases are considered to monitor the code ability to solve for the diffusive and turbulent fluxes, and the chemical source term. In addition, the code is validated by resolving the transverse sonic injection into supersonic air flow in the case of Helium injection from a flat plate, and in the case of Hydrogen injection in a single-strut scramjet engine. The effectiveness of this injection technique in mixing and flame-holding is demonstrated. The results show good agreement with the previous numerical and experimental investigations, and prove the simulator's accuracy.
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About the Author
Mohammed Kamel is a Lecturer Assistant in Cairo University, Faculty of Engineering, Aerospace Engineering Department, where he obtained the M.Sc. degree in Aerospace Propulsion. He is pursing his PhD study in the University of Notre Dame. He has expertise in Computational Fluid Mechanics, Turbulence Modeling, Reacting-Flows, and Aeroacoustics.
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Towards a Numerical Simulation of Supersonic Mixing & Combustion
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LAP LAMBERT Academic Publishing Aug 2013, 2013
ISBN 10: 3659387045
ISBN 13: 9783659387043
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Taschenbuch. Condition: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -The design and off-design studies of the hypersonic air-breathing engines face many challenges, due to the complexity of their internal flows. The mixing and combustion processes in Supersonic-Combustion Ramjet (scramjet) engines involve complicated aerothermochemical features, such as: the interactions between shock-waves and boundary-layer, the shock induced-combustion and the recirculation zones. In this study, a numerical solver is developed and validated to be an efficient design tool capable of simulating these complicated flow features of the supersonic combustors. For the code validation, several test cases are considered to monitor the code ability to solve for the diffusive and turbulent fluxes, and the chemical source term. In addition, the code is validated by resolving the transverse sonic injection into supersonic air flow in the case of Helium injection from a flat plate, and in the case of Hydrogen injection in a single-strut scramjet engine. The effectiveness of this injection technique in mixing and flame-holding is demonstrated. The results show good agreement with the previous numerical and experimental investigations, and prove the simulator's accuracy. 208 pp. Englisch. Seller Inventory # 9783659387043
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Towards a Numerical Simulation of Supersonic Mixing & Combustion
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Condition: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Kamel MohammedMohammed Kamel is a Lecturer Assistant in Cairo University, Faculty of Engineering, Aerospace Engineering Department, where he obtained the M.Sc. degree in Aerospace Propulsion. He is pursing his PhD study in the Univer. Seller Inventory # 5152855
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Towards a Numerical Simulation of Supersonic Mixing & Combustion | Development & Validation of a Computational Solver for Two-Dimensional Compressible Chemically-Reacting Turbulent Flows
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Taschenbuch. Condition: Neu. Towards a Numerical Simulation of Supersonic Mixing & Combustion | Development & Validation of a Computational Solver for Two-Dimensional Compressible Chemically-Reacting Turbulent Flows | Mohammed Kamel (u. a.) | Taschenbuch | 208 S. | Englisch | 2013 | LAP LAMBERT Academic Publishing | EAN 9783659387043 | Verantwortliche Person für die EU: BoD - Books on Demand, In de Tarpen 42, 22848 Norderstedt, info[at]bod[dot]de | Anbieter: preigu. Seller Inventory # 105710731
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Towards a Numerical Simulation of Supersonic Mixing & Combustion
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LAP LAMBERT Academic Publishing Aug 2013, 2013
ISBN 10: 3659387045
ISBN 13: 9783659387043
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Taschenbuch. Condition: Neu. This item is printed on demand - Print on Demand Titel. Neuware -The design and off-design studies of the hypersonic air-breathing engines face many challenges, due to the complexity of their internal flows. The mixing and combustion processes in Supersonic-Combustion Ramjet (scramjet) engines involve complicated aerothermochemical features, such as: the interactions between shock-waves and boundary-layer, the shock induced-combustion and the recirculation zones. In this study, a numerical solver is developed and validated to be an efficient design tool capable of simulating these complicated flow features of the supersonic combustors. For the code validation, several test cases are considered to monitor the code ability to solve for the diffusive and turbulent fluxes, and the chemical source term. In addition, the code is validated by resolving the transverse sonic injection into supersonic air flow in the case of Helium injection from a flat plate, and in the case of Hydrogen injection in a single-strut scramjet engine. The effectiveness of this injection technique in mixing and flame-holding is demonstrated. The results show good agreement with the previous numerical and experimental investigations, and prove the simulator's accuracy.Books on Demand GmbH, Überseering 33, 22297 Hamburg 208 pp. Englisch. Seller Inventory # 9783659387043
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Towards a Numerical Simulation of Supersonic Mixing & Combustion : Development & Validation of a Computational Solver for Two-Dimensional Compressible Chemically-Reacting Turbulent Flows
Published by
LAP LAMBERT Academic Publishing, 2013
ISBN 10: 3659387045
ISBN 13: 9783659387043
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Taschenbuch. Condition: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - The design and off-design studies of the hypersonic air-breathing engines face many challenges, due to the complexity of their internal flows. The mixing and combustion processes in Supersonic-Combustion Ramjet (scramjet) engines involve complicated aerothermochemical features, such as: the interactions between shock-waves and boundary-layer, the shock induced-combustion and the recirculation zones. In this study, a numerical solver is developed and validated to be an efficient design tool capable of simulating these complicated flow features of the supersonic combustors. For the code validation, several test cases are considered to monitor the code ability to solve for the diffusive and turbulent fluxes, and the chemical source term. In addition, the code is validated by resolving the transverse sonic injection into supersonic air flow in the case of Helium injection from a flat plate, and in the case of Hydrogen injection in a single-strut scramjet engine. The effectiveness of this injection technique in mixing and flame-holding is demonstrated. The results show good agreement with the previous numerical and experimental investigations, and prove the simulator's accuracy. Seller Inventory # 9783659387043