Research On Supersonic Turbulent Separated And Reattached Flows
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Research On Supersonic Turbulent Separated And Reattached Flows
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Author : Seymour M. Bogdonoff
language : en
Publisher:
Release Date : 1975
Research On Supersonic Turbulent Separated And Reattached Flows written by Seymour M. Bogdonoff and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1975 with Aerodynamics, Supersonic categories.
Basic research programs are reported with fundamental applications to supersonic flight. The experimental studies made use of the unique capabilities of the high Reynolds number Mach 3 facility. The experimental programs concentrated on phenomena associated with incipient separation and separation of turbulent boundary layers over a large Reynolds number range. The reattachment phenomena of a shear layer was also studied in great depth.
Research On Supersonic Turbulent Separated And Reattached Flows
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Author : S. M. Bogdonoff
language : en
Publisher:
Release Date : 1975
Research On Supersonic Turbulent Separated And Reattached Flows written by S. M. Bogdonoff and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1975 with categories.
Basic research programs are reported with fundamental applications to supersonic flight. The experimental studies made use of the unique capabilities of the high Reynolds number Mach 3 facility. The experimental programs concentrated on phenomena associated with incipient separation and separation of turbulent boundary layers over a large Reynolds number range. The reattachment phenomena of a shear layer was also studied in great depth.
Research On Supersonic Turbulent Separated And Reattached Flows
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Author : S. M. Bogdonoff
language : en
Publisher:
Release Date : 1975
Research On Supersonic Turbulent Separated And Reattached Flows written by S. M. Bogdonoff and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1975 with categories.
Basic research programs are reported with fundamental applications to supersonic flight. The experimental studies made use of the unique capabilities of the high Reynolds number Mach 3 facility. The experimental programs concentrated on phenomena associated with incipient separation and separation of turbulent boundary layers over a large Reynolds number range. The reattachment phenomena of a shear layer was also studied in great depth.
Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date : 1995
Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1995 with Aeronautics categories.
Separation Of Flow
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Author : Paul K. Chang
language : en
Publisher: Elsevier
Release Date : 2014-06-28
Separation Of Flow written by Paul K. Chang and has been published by Elsevier this book supported file pdf, txt, epub, kindle and other format this book has been release on 2014-06-28 with Technology & Engineering categories.
Interdisciplinary and Advanced Topics in Science and Engineering, Volume 3: Separation of Flow presents the problem of the separation of fluid flow. This book provides information covering the fields of basic physical processes, analyses, and experiments concerning flow separation. Organized into 12 chapters, this volume begins with an overview of the flow separation on the body surface as discusses in various classical examples. This text then examines the analytical and experimental results of the laminar boundary layer of steady, two-dimensional flows in the subsonic speed range. Other chapters consider the study of flow separation on the two-dimensional body, flow separation on three-dimensional body shape and particularly on bodies of revolution. This book discusses as well the analytical solutions of the unsteady flow separation. The final chapter deals with the purpose of separation flow control to raise efficiency or to enhance the performance of vehicles and fluid machineries involving various engineering applications. This book is a valuable resource for engineers.
Nbs Special Publication
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Author :
language : en
Publisher:
Release Date : 1968
Nbs Special Publication written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1968 with Weights and measures categories.
Experimental Separation Studies For Two Dimensional Wedges And Curved Surfaces At Mach Numbers Of 4 8 To 6 2
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Author : James R. Sterrett
language : en
Publisher:
Release Date : 1962
Experimental Separation Studies For Two Dimensional Wedges And Curved Surfaces At Mach Numbers Of 4 8 To 6 2 written by James R. Sterrett and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1962 with Aerodynamics, Hypersonic categories.
Shock Wave Boundary Layer Interactions
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Author : Holger Babinsky
language : en
Publisher: Cambridge University Press
Release Date : 2011-09-12
Shock Wave Boundary Layer Interactions written by Holger Babinsky and has been published by Cambridge University Press this book supported file pdf, txt, epub, kindle and other format this book has been release on 2011-09-12 with Technology & Engineering categories.
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.
Separated Flows
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Author : North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Fluid Dynamics Panel
language : en
Publisher:
Release Date : 1966
Separated Flows written by North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Fluid Dynamics Panel and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1966 with Aerodynamics, Hypersonic categories.
Method For Calculating Effects Of Dissociation On Flow Variables In The Relaxation Zone Behind Normal Shock Waves
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Author : John S. Evans
language : en
Publisher:
Release Date : 1956
Method For Calculating Effects Of Dissociation On Flow Variables In The Relaxation Zone Behind Normal Shock Waves written by John S. Evans and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1956 with Air flow categories.
Because the chemical reaction rates needed to predict the dependence of degree of dissociation on distance behind the shock are not known, order-of-magnitude estimates of their values have been used in a numerical example, the purpose of which is to illustrate the use of reaction-rate equations to predict relaxation time and distance behind the shock front.