Hypersonic shock wave turbulent boundary layers :direct numerical simulation, large eddy simulation and experiment /

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"Version: 202306"--Title page verso.Includes bibliographical references.1. Introduction -- 2. Mathematical theory -- 2.1. Navier-Stokes equations -- 2.2. Reynolds-averaged Navier-Stokes equations -- 2.3. Turbulent Prandtl and Lewis numbers -- 2.4. Large Eddy Simulation -- 2.5. Inflow boundary conditions -- 2.6. Reynolds number dependence3. Equilibrium turbulent boundary layers -- 3.1. Incompressible law of the wall and wake -- 3.2. Compressible velocity transformations -- 3.3. Mean velocity-mean temperature relations -- 3.4. Reynolds analogy factor -- 3.5. Morkovin's hypothesis -- 3.6. Morkovin's strong Reynolds analogies -- 3.7. Cebeci and Smith strong Reynolds analogy -- 3.8. Huang et al strong Reynolds analogy -- 4. Experiments--hypersonic turbulent boundary layers -- 5. Experiments--hypersonic shock wave turbulent boundary layer interactions -- 6. Direct numerical simulation and large eddy simulation--boundary layers -- 7. Direct numerical simulation and large eddy simulation--shock boundary layer interaction8. Discussion and future needs -- 8.1. Equilibrium turbulent boundary layer -- 8.2. Shock wave boundary layer interaction -- 8.3. Summary -- Appendix A. Hypersonic test facilities.Hypersonic turbulent boundary layers are a fundamental phenomenon in high-speed flight. The interaction of shock waves with hypersonic turbulent boundary layers has a critical impact on vehicle aerothermodynamic loading including surface heat transfer, pressure and skin friction. This book provides a comprehensive exposition of hypersonic turbulent boundary layers, including the fundamental mathematical theory, structure of equilibrium boundary layers, and extensive surveys of Direct Numerical Simulation (DNS), Large Eddy Simulation (LES) and experiments. It also provides a roadmap for both future experiments and DNS and LES simulations. Descriptions of hypersonic ground test facilities is included as an appendix. As a research and reference text, this book would appeal to graduate students and researchers in hypersonics and could be the basis for professional training courses.Graduate students and researchers (academia, industry, government laboratories) in hypersonics.Also available in print.Mode of access: World Wide Web.System requirements: Adobe Acrobat Reader, EPUB reader, or Kindle reader.Doyle Knight is Distinguished Professor of Aerospace Engineering at Rutgers, The State University of New Jersey. He is the author of more than one hundred journal papers, over 200 conference papers, and two books. His research in gas dynamics includes supersonic and hypersonic shock wave boundary layer interaction, turbulence model development, high-speed inlet unstart and effects of unsteady energy deposition in high-speed flows. His research activity in design optimization focuses on the application of computational fluid dynamics to the automated optimal design of high-speed air vehicles. Nadia Kianvashrad is Postdoctoral Associate in the Department of Mechanical and Aerospace Engineering at Rutgers, The State University of New Jersey. She is the author of six journal papers and 20 conference papers. Her research interests include computational gas dynamics. Her research in computational gas dynamics includes laminar and turbulent shock wave boundary layer interaction in hypersonic flows, and energy deposition for flow and flight control in supersonic and hypersonic flows.Title from PDF title page (viewed on July 6, 2023).

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Publisher

: .,

Collation

1 online resource (various pagings) :illustrations.

Language

English

ISBN/ISSN

9780750350020

Classification

531.1133

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Edition

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Subject(s)

Shock waves.
Fluid mechanics.
Turbulent boundary layer.
Shock waves
Turbulent boundary layer
SCIENCE / Mechanics / Aerodynamics.

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Doyle Knight and Nadia Kianvashrad.

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