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EBookClubs

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Book Documentation of Two  and Three dimensional Hypersonic Shock Wave turbulent Boundary Layer Interaction Flows

Download or read book Documentation of Two and Three dimensional Hypersonic Shock Wave turbulent Boundary Layer Interaction Flows written by Marvin I. Kussoy and published by . This book was released on 1989 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Hypersonic Shock Wave Turbulent Boundary Layers

Download or read book Hypersonic Shock Wave Turbulent Boundary Layers written by Doyle Knight and published by . This book was released on 2023 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.

Book Shock Wave Boundary Layer Interactions

Download or read book Shock Wave Boundary Layer Interactions written by Holger Babinsky and published by Cambridge University Press. This book was released on 2011-09-12 with total page 481 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.

Book Expansion Corner Effects on Hypersonic Shock Wave turbulent Boundary Layer Interactions

Download or read book Expansion Corner Effects on Hypersonic Shock Wave turbulent Boundary Layer Interactions written by Michael E. White and published by . This book was released on 1996 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Prediction of Hypersonic Shock wave turbulent boundary layer Interaction Flows

Download or read book Prediction of Hypersonic Shock wave turbulent boundary layer Interaction Flows written by C.C. Horstman and published by . This book was released on 1987 with total page 10 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Hypersonic Shock Wave turbulent Boundary Layer Interactions on a Porous Surface

Download or read book Hypersonic Shock Wave turbulent Boundary Layer Interactions on a Porous Surface written by Rebecca L. Hanna and published by . This book was released on 1995 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Hypersonic Shock wave Turbulent Boundary Layer Interaction Flows

Download or read book Hypersonic Shock wave Turbulent Boundary Layer Interaction Flows written by C. C. Horstmann and published by . This book was released on 1991 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Documentation of Two  And Three Dimensional Hypersonic Shock Wave Turbulent Boundary Layer Interaction Flows

Download or read book Documentation of Two And Three Dimensional Hypersonic Shock Wave Turbulent Boundary Layer Interaction Flows written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-02 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: Experimental data for a series of two- and three-dimensional shock wave/turbulent boundary layer interaction flows at Mach 7 are presented. Test bodies, composed of simple geometric shapes, were designed to generate flows with varying degrees of pressure gradient, boundary-layer separation, and turning angle. The data include surface-pressure and heat-transfer distributions as well as limited mean-flow-field surveys in both the undisturbed and the interaction regimes. The data are presented in a convenient form for use in validating existing or future computational models of these generic hypersonic flows. Kussoy, Marvin I. and Horstman, Clifford C. Ames Research Center NCC2-452; RTOP 505-80-11...

Book Hypersonic Crossing Shock wave turbulent Boundary Layer Interactions

Download or read book Hypersonic Crossing Shock wave turbulent Boundary Layer Interactions written by M. I. Kussoy and published by . This book was released on 1993 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Shock Wave Turbulent Boundary Layer Interaction in Hypersonic Flow

Download or read book Shock Wave Turbulent Boundary Layer Interaction in Hypersonic Flow written by Michael S. Holden and published by . This book was released on 1975 with total page 185 pages. Available in PDF, EPUB and Kindle. Book excerpt: A study is presented of the characteristics of transitional and turbulent layers, and regions of shock wave-turbulent boundary layer interaction in high Reynolds number hypersonic flow. An examination and correlation of skin friction, heat transfer and pressure measurements in laminar, transitional and turbulent boundary layers on sharp flat plates and cones are presented for the Mach range from 3 to 13 at wall-to-free stream temperature ratios from 0.1 to 0.4.