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ISBN 13: 9780521848527

It is a valuable resource for the specialist because it gathers experimental, computational and theoretical knowledge in one place. 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. From to , 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.

Reattachment heating upstream of short compression ramps in hypersonic flow | SpringerLink

He joined the Engineering Department at Cambridge University in 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.

He serves on a number of national and international advisory bodies. He has developed undergraduate- and graduate-level courses in Fluid Mechanics and received several awards for his teaching. Convert currency. Add to Basket. Compare all 14 new copies. Book Description Cambridge University Press, Condition: New. More information about this seller Contact this seller. Language: English. Brand new Book.

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.

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Using this site means you agree to our use of cookies. View cookies policy. Zoom Zoom. Harvey Contributor. Availability Special Order item not currently available. We'll try and order for you. With Free Saver Delivery. Zheltovodov and Doyle D. Knight; 5.

Professor Yufeng Yao

Ideal gas shock wave turbulent boundary layer interactions in supersonic flows and their modeling - three dimensional interactions Doyle D. Knight and Alexander A. Zheltovodov; 6. Holden; 7.

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Numerical simulation of hypersonic shock wave boundary layer interactions Graham V. Candler; 8. Harvey; 9. Shock wave unsteadiness in turbulent shock wave boundary layer interactions P. Dupont, J. Debieve and J. Dussauge; Review quote ' Riley, Contemporary Physics 'A welcome addition to the literature on high-speed flows, this volume assembles nine technical chapters by experts in specific and generic problems of shock-wave interactions with boundary layers that continue to challenge experiment, numerical simulation and modelling Riley, Contemporary Physics Today "A welcome addition to the literature on high-speed flows, this volume assembles nine technical chapters by experts in specific and generic problems of shock-wave interactions with boundary layers that continue to challenge experiment, numerical simulation and modelling From to , 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 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.

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He serves on a number of national and international advisory bodies. He has developed undergraduate- and graduate-level courses in Fluid Mechanics and received several awards for his teaching. John K. He obtained his PhD in at Imperial College for research into the roll stability of slender delta wings which was an integral part of the Concorde development program.


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In the early s he became involved in experimental research into rarefied hypersonic flows, initially with Professor Bogdonoff at Princeton University and subsequently back at Imperial College in London. He has published widely on the use of the Direct Simulation Monte Carlo DSMC computational method to predict low density flows and he has specialized in the development of suitable molecular collision models used in these computations to represent reacting, ionized and thermally radiating gases.