05511nam a2200625 i 45000010014000000030004000140050017000180060019000350070015000540080041000690200025001100200024001350200025001590200027001840240035002110350025002460350022002710400040002930500030003330720017003630720023003801000028004032450160004312640098005913000058006893360021007473370026007683380032007944900027008264900034008535000041008875040041009285050272009695050694012415050185019355200895021205210100030155300029031155380036031445380078031805451097032585880056043556500017044116500030044286500038044586500051044966500029045476500049045767000033046257100054046587760049047128300031047618300034047928560059048269780750350020IOP20251030124215.0m    eo  d        cr bn |||m|||a230701s2023    enka   fob    000 0 eng d  a9780750350020qebook  a9780750350013qmobi  z9780750350006qprint  z9780750350037qmyPrint7 a10.1088/978-0-7503-5002-02doi  a(CaBNVSL)thg00083631  a(OCoLC)1389632629  aCaBNVSLbengerdacCaBNVSLdCaBNVSL 4aQC168.85.S45bK655 2023eb 7aPHDF2bicssc 7aSCI0840002bisacsh1 aKnight, Doyle,eauthor.10aHypersonic shock wave turbulent boundary layers :bdirect numerical simulation, large eddy simulation and experiment /cDoyle Knight and Nadia Kianvashrad. 1aBristol [England] (Temple Circus, Temple Way, Bristol BS1 6HG, UK) :bIOP Publishing,c[2023]  a1 online resource (various pagings) :billustrations.  atext2rdacontent  aelectronic2isbdmedia  aonline resource2rdacarrier1 a[IOP release $release]1 aIOP ebooks. [2023 collection]  a"Version: 202306"--Title page verso.  aIncludes bibliographical references.0 a1. 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 dependence8 a3. 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 a8. 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.3 aHypersonic 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.  aGraduate students and researchers (academia, industry, government laboratories) in hypersonics.  aAlso available in print.  aMode of access: World Wide Web.  aSystem requirements: Adobe Acrobat Reader, EPUB reader, or Kindle reader.  aDoyle 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.0 aTitle from PDF title page (viewed on July 6, 2023). 0aShock waves. 0aTurbulent boundary layer. 0aShock wavesxComputer simulation. 0aTurbulent boundary layerxComputer simulation. 7aFluid mechanics.2bicssc 7aSCIENCE / Mechanics / Aerodynamics.2bisacsh1 aKianvashrad, Nadia,eauthor.2 aInstitute of Physics (Great Britain),epublisher.08iPrint version:z9780750350006z9780750350037 0aIOP (Series).pRelease 23. 0aIOP ebooks.p2023 collection.40uhttps://iopscience.iop.org/book/mono/978-0-7503-5002-0