Shock Wave-Boundary-Layer Interactions (Cambridge Aerospace Series)

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9780521848527: Shock Wave-Boundary-Layer Interactions (Cambridge Aerospace Series)
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Shock Wave/Boundary Layer Interaction (SBLI) is a fundamental phenomenon in gasdynamics and frequently a defining feature in high speed aerodynamic flowfields. The interactions can be found in practical situations, ranging from transonic aircraft wings to hypersonic vehicles and engines. SBLI's have the potential to pose serious problems and is thus a critical issue for aerospace applications. This is the first book devoted solely to a comprehensive, state of the art explanation of the phenomenon with coverage of all flow regimes where SBLI's occur. The book includes contributions from leading international experts who share their insight into SBLI physics and the impact of these interactions on practical flow situations. This book is aimed at practitioners and graduate students in aerodynamics who wish to familiarise themselves with all aspects of SBLI flows. It is a valuable resource for the specialist because it gathers experimental, computational and theoretical knowledge in one place.

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Shock Wave/Boundary Layer Interaction (SBLI) is a fundamental phenomenon in gasdynamics and frequently a defining feature in high speed aerodynamic flowfields. This is the first book devoted solely to the phenomenon and covers all flow regimes where SBLI's occur. The contributions are from international experts sharing their insights into SBLI physics and practical flow situations.

About the Author:

Holger Babinsky is Professor of Aerodynamics at the University of Cambridge and a Fellow of Magdalene College. He received his Diplom-Ingenieur (German equivalent of MS degree) with distinction from the University of Stuttgart and his PhD from Cranfield University with an experimental study of roughness effects on hypersonic SBLIs. From 1994 to 1995, he was a Research Associate at the Shock Wave Research Centre of Tohoku University, Japan, where he worked on experimental and numerical investigations of shock-wave dynamics. He joined the Engineering Department at Cambridge University in 1995 to supervise research in its high-speed flow facilities. Professor Babinsky has twenty years experience in the research of SBLIs, particularly in the development of flow-control techniques to mitigate the detrimental impact of such interactions. He has authored and coauthored many experimental and theoretical articles on high-speed flows, SBLIs and flow control, as well as various low-speed aerodynamics subjects. Professor Babinsky is a Fellow of the Royal Aeronautical Society, an Associate Fellow of the American Institute of Aeronautics and Astronautics (AIAA) and a Member of the International Shock Wave Institute. He serves on a number of national and international advisory bodies. Recently, in collaboration with the US Air Force Research Laboratories, he organized the first AIAA workshop on shock wave-boundary-layer prediction. He has developed undergraduate- and graduate-level courses in Fluid Mechanics and received several awards for his teaching.

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9781107646537: Shock Wave-Boundary-Layer Interactions (Cambridge Aerospace Series)

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ISBN 10:  1107646537 ISBN 13:  9781107646537
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Book Description CAMBRIDGE UNIVERSITY PRESS, United Kingdom, 2013. Hardback. Condition: New. Language: English . Brand New Book ***** Print on Demand *****. Shock wave-boundary-layer interaction (SBLI) is a fundamental phenomenon in gas dynamics that is observed in many practical situations, ranging from transonic aircraft wings to hypersonic vehicles and engines. SBLIs have the potential to pose serious problems in a flowfield; hence they often prove to be a critical - or even design limiting - issue for many aerospace applications. This is the first book devoted solely to a comprehensive, state-of-the-art explanation of this phenomenon. It includes a description of the basic fluid mechanics of SBLIs plus contributions from leading international experts who share their insight into their physics and the impact they have in practical flow situations. This book is for practitioners and graduate students in aerodynamics who wish to familiarize themselves with all aspects of SBLI flows. It is a valuable resource for specialists because it compiles experimental, computational and theoretical knowledge in one place. Seller Inventory # APC9780521848527

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Book Description CAMBRIDGE UNIVERSITY PRESS, United Kingdom, 2013. Hardback. Condition: New. Language: English . Brand New Book ***** Print on Demand *****.Shock wave-boundary-layer interaction (SBLI) is a fundamental phenomenon in gas dynamics that is observed in many practical situations, ranging from transonic aircraft wings to hypersonic vehicles and engines. SBLIs have the potential to pose serious problems in a flowfield; hence they often prove to be a critical - or even design limiting - issue for many aerospace applications. This is the first book devoted solely to a comprehensive, state-of-the-art explanation of this phenomenon. It includes a description of the basic fluid mechanics of SBLIs plus contributions from leading international experts who share their insight into their physics and the impact they have in practical flow situations. This book is for practitioners and graduate students in aerodynamics who wish to familiarize themselves with all aspects of SBLI flows. It is a valuable resource for specialists because it compiles experimental, computational and theoretical knowledge in one place. Seller Inventory # APC9780521848527

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