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Hypersonic Shock Wave Turbulent Boundary Layer Interactions On A Porous Surface
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Book Synopsis Hypersonic Shock Wave/turbulent Boundary Layer Interactions on a Porous Surface by : Rebecca L. Hanna
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 Synopsis Documentation of Two- and Three-dimensional Hypersonic Shock Wave/turbulent Boundary Layer Interaction Flows by : Marvin I. Kussoy
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 Synopsis Hypersonic Shock Wave/turbulent Boundary Layer Interactions in the Vicinity of an Expansion Corner by : Michael E. White
Download or read book Hypersonic Shock Wave/turbulent Boundary Layer Interactions in the Vicinity of an Expansion Corner written by Michael E. White and published by . This book was released on 1995 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Experimental Documentation of a Hypersonic Shock-wave Turbulent Boundary Layer Interaction Flow: With and Without Separation by :
Download or read book An Experimental Documentation of a Hypersonic Shock-wave Turbulent Boundary Layer Interaction Flow: With and Without Separation written by and published by . This book was released on 1975 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Prediction of Hypersonic Shock-wave/turbulent-boundary-layer Interaction Flows by : C.C. Horstman
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:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722182298 Total Pages :28 pages Book Rating :4.1/5 (822 download)
Book Synopsis Documentation of Two- And Three-Dimensional Hypersonic Shock Wave/Turbulent Boundary Layer Interaction Flows by : National Aeronautics and Space Administration (NASA)
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 Synopsis Hypersonic Shock-wave Turbulent Boundary Layer Interaction Flows by : C. C. Horstmann
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 Synopsis The Hypersonic Shock Wave-turbulent Boundary Layer Interaction Generated by a Sharp Fin at Mach 8.2 by : Doyle D. Knight
Download or read book The Hypersonic Shock Wave-turbulent Boundary Layer Interaction Generated by a Sharp Fin at Mach 8.2 written by Doyle D. Knight and published by . This book was released on 1992 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Expansion Corner Effects on Hypersonic Shock Wave/turbulent Boundary Layer Interactions by : Michael E. White
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 Synopsis Hypersonic Crossing Shock-wave/turbulent Boundary Layer Interactions by : M. I. Kussoy
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 Synopsis Experimental investigations of supersonic and hypersonic shock wave/turbulent boundary layer interactions by : Anne-Marie Schreyer
Download or read book Experimental investigations of supersonic and hypersonic shock wave/turbulent boundary layer interactions written by Anne-Marie Schreyer and published by . This book was released on 2012 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Shock Wave - Turbulent Boundary Layer Interaction in Hypersonic Flow by : M. S. Holden
Download or read book Shock Wave - Turbulent Boundary Layer Interaction in Hypersonic Flow written by M. S. Holden and published by . This book was released on 1973 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Shock Wave-Boundary-Layer Interactions by : Holger Babinsky
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 Synopsis Shock Wave/Turbulent Boundary Layer Interaction in High-Reynolds-Number Hypersonic Flows by :
Download or read book Shock Wave/Turbulent Boundary Layer Interaction in High-Reynolds-Number Hypersonic Flows written by and published by . This book was released on 1987 with total page 152 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report investigated fundamental aerothermal phenomena in hypersonic flow, with particular emphasis on viscous/inviscid interaction phenomena. The experimental studies were conducted to examine the changes in the structure at the base of a hypersonic turbulent boundary layer as it is subjected to a strong self-induced pressure gradient in regions of shock wave/ boundary layer interaction. The initial phase of the theoretical program was directed toward summarizing existing techniques for obtaining Navier/Stokes solutions for laminar flow over flat plates in hypersonic flow. In the experimental program, surface and flow field measurements were made to examine the detailed flow mechanics associated with turbulent boundary layer separation over a large cone flare model at Mach numbers 11, 13 and 16 and Reynolds numbers up to 100 million. Holography measurements were used to examine the flow field regions of hypersonic shock wave/turbulent boundary layer interaction. In this preliminary investigation of the application of holography in a 96 inch Shock Tunnel, holographic interferograms were obtained for viscous/inviscid interactions at Mach numbers 11 and 13 and Reynolds numbers up to 30 million, nominally. Flow field studies were made for flat plate/wedge, cone/flare and incident shock configurations. The quantitative results presented offer new information as well as a potential to obtain density measurements in other types of hypersonic flow; however, they also reveal important concerns which need to be resolved before the interferometric data can be claimed to give accurate measurements of these flows. Two appendices include an invited review paper on aerothermal problems associated with hypersonic flight.
Book Synopsis Shock Wave - Turbulent Boundary Layer Interaction in Hypersonic Flow by : Michael S. Holden
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 1973 with total page 69 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Supersonic Shock Wave-turbulent Boundary Layer Interactions by : C. Herbert Law
Download or read book Supersonic Shock Wave-turbulent Boundary Layer Interactions written by C. Herbert Law and published by . This book was released on 1975 with total page 7 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Hypersonic Shock Wave Turbulent Boundary Layers by : Doyle Knight
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.