TY  - BOOK
AU  - Knight,Doyle
AU  - Kianvashrad,Nadia
ED  - Institute of Physics (Great Britain),
TI  - Hypersonic shock wave turbulent boundary layers: direct numerical simulation, large eddy simulation and experiment 
T2  - [IOP release $release]
SN  - 9780750350020
AV  - QC168.85.S45 K655 2023eb
PY  - 2023///]
CY  - Bristol [England] (Temple Circus, Temple Way, Bristol BS1 6HG, UK)
PB  - IOP Publishing
KW  - Shock waves
KW  - Turbulent boundary layer
KW  - Computer simulation
KW  - Fluid mechanics
KW  - bicssc
KW  - SCIENCE / Mechanics / Aerodynamics
KW  - bisacsh
N1  - "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 dependence; 3. 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 interaction; 8. 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; Graduate students and researchers (academia, industry, government laboratories) in hypersonics; Also available in print
N2  - 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
UR  - https://iopscience.iop.org/book/mono/978-0-7503-5002-0
ER  -