Incipient Separation Of A Turbulent Boundary Layer At High Reynolds Number In Two Dimensional Supersonic Flow Over A Compression Corner
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Two Dimensional Compression Corner And Planar Shock Wave Interactions With A Supersonic Turbulent Boundary Layer
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Author : C. Herbert Law
language : en
Publisher:
Release Date : 1975
Two Dimensional Compression Corner And Planar Shock Wave Interactions With A Supersonic Turbulent Boundary Layer written by C. Herbert Law and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1975 with Aerodynamic load categories.
Incipient Separation Of A Turbulent Boundary Layer At High Reynolds Number In Two Dimensional Supersonic Flow Over A Compression Corner
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Author :
language : en
Publisher:
Release Date : 1969
Incipient Separation Of A Turbulent Boundary Layer At High Reynolds Number In Two Dimensional Supersonic Flow Over A Compression Corner written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1969 with categories.
Nasa Technical Report
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Author :
language : en
Publisher:
Release Date : 1961
Nasa Technical Report written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Aerodynamics categories.
Turbulent Boundary Layer Separation Induced By Flares On Cylinders At Zero Angle Of Attack
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Author : Donald M. Kuehn
language : en
Publisher:
Release Date : 1961
Turbulent Boundary Layer Separation Induced By Flares On Cylinders At Zero Angle Of Attack written by Donald M. Kuehn and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Noses (Space vehicles) categories.
Separation caused by the pressure rise induced by flares has been experimentally investigated in the Mach number range of 1.5 to 5.0 and in the Reynolds number range (based on boundary-layer thickness) of 1.5X104 to 12X104. The purpose of the investigation was to determine the model geometry and flow conditions for which separation can be expected for a turbulent boundary layer of zero pressure gradient on the cylinder approaching the flare. Comparisons are made of the boundary-layer-separation characteristics of these three-dimensional flares with two-dimensional separation results from a previous investigation.
Experimental Study On High Subsonic Turbulent Flow Incipient Separation
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Author : Jain-Ming Wu
language : en
Publisher:
Release Date : 1976
Experimental Study On High Subsonic Turbulent Flow Incipient Separation written by Jain-Ming Wu and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1976 with Aerodynamics categories.
For flow over a two-dimensional ramp compression corner case, an experimental investigation to determine the incipient separation was carried out at Mach numbers between 0.55 and 0.9 and Reynolds numbers (based on undisturbed boundary layer thickness) between 350,000 and 690,000. Detailed surface pressure, pitot traversing and oil flow data were obtained for each ramp angle case. Two-dimensionality of the ramp compression corners was verified by the surface oil flow. A major finding of this study is that the incipient separation ramp angle is relatively independent of Mach number and Reynolds number within the range studied. The incipient separation ramp angle was found to be about 22.5 degrees.
Scramjet Propulsion
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Author : E. T. Curran
language : en
Publisher: AIAA
Release Date : 2000
Scramjet Propulsion written by E. T. Curran and has been published by AIAA this book supported file pdf, txt, epub, kindle and other format this book has been release on 2000 with Airplanes 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.
Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date : 1986
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 1986 with Aeronautics categories.
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.
Separated Flows And Jets
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Author : Victor V. Kozlov
language : en
Publisher: Springer Science & Business Media
Release Date : 2012-12-06
Separated Flows And Jets written by Victor V. Kozlov and has been published by Springer Science & Business Media this book supported file pdf, txt, epub, kindle and other format this book has been release on 2012-12-06 with Science categories.
Separated flows and jets are closely linked in a variety of applications. They are of great importance in various fields of fluid mechanics including vehicle efficiency, technical branches concerned with gas/liquid flows, atmospheric effects on various constructions, etc. Knowledge of the physics of separated flows and jets and the development of reliable control techniques are prerequisite for future progress in the field. These aspects were in focus during the IUTAM-Symposium which was held in Novosibirsk, 9-13 July, 1990. This volume contains a selection of papers presenting recent results of theoretical and numerical studies as well as experimental work on separated flows and jets. The topics include sub- and supersonic, laminar and turbulent separation as well as organized structures in separated flows and jets. The reader will find here the state of the art and major trends for research in this field of aero-hydrodynamics.