Some Effects Of Shock Induced Separation Of Turbulent Boundary Layers In Transonic Flow Past Aerofoils
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Author | : H. H. Pearcey |
Publisher | : |
Total Pages | : |
Release | : 1955 |
Genre | : |
ISBN | : |
Download Some Effects of Shock-induced Separation of Turbulent Boundary Layers in Transonic Flow Past Aerofoils Book in PDF, Epub and Kindle
Author | : Aeronautical Research Council (Great Britain) |
Publisher | : |
Total Pages | : 61 |
Release | : 1959 |
Genre | : Aerofoils |
ISBN | : |
Download Some Effects of Shock-induced Separation of Turbulent Boundary Layers in Transonic Flow Past Aerofoils Book in PDF, Epub and Kindle
Author | : Aeronautical Research Council (Great Britain) |
Publisher | : |
Total Pages | : 61 |
Release | : 1959 |
Genre | : |
ISBN | : |
Download Some Effects of Shock-induced Separations of Turbulent Boundary Layers in Transonic Flow Past Aerofoils Book in PDF, Epub and Kindle
Author | : H. H. Pearcey |
Publisher | : |
Total Pages | : 61 |
Release | : 1959 |
Genre | : |
ISBN | : |
Download Some Effects of Shock-induced Separation of Turbulent Boundary Layers in Transinic Flow Past Aerofoils Book in PDF, Epub and Kindle
Author | : Anthony W. Fiore |
Publisher | : |
Total Pages | : 962 |
Release | : 1978 |
Genre | : Turbulent boundary layer |
ISBN | : |
Download Boundary Layer Effects Book in PDF, Epub and Kindle
In 1975 the U.S. Air Force and the Federal Republic of Germany signed a Data Exchange Agreement numbered AF-75-G-7440 entitled 'Viscous and Interacting Flow Fields.' The purpose was to exchange data in the area of boundary layer research. It includes both experimental and theoretical boundary layer research at speeds from subsonic to hypersonic Mach numbers in the presence of laminar, transitional, and turbulent boundary layers. The main effort in recent years has been on turbulent boundary layers, both attached and separated in the presence of such parameters as pressure gradients, wall temperature, surface roughness, etc. In the United States the research was conducted in various Department of Defense, NASA, aircraft corporations, and various university laboratories. In the Federal Republic of Germany it was carried out within the various DFVLR, industrial, and university research centers.
Author | : Holger Babinsky |
Publisher | : Cambridge University Press |
Total Pages | : 481 |
Release | : 2011-09-12 |
Genre | : Technology & Engineering |
ISBN | : 1139498649 |
Download Shock Wave-Boundary-Layer Interactions Book in PDF, Epub and Kindle
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.
Author | : Eugene S. Love |
Publisher | : |
Total Pages | : 702 |
Release | : 1955 |
Genre | : Aerodynamic load |
ISBN | : |
Download Pressure Rise Associated with Shock-induced Boundary-layer Separation Book in PDF, Epub and Kindle
Some recent contributions to the problem of shock-induced separation of the boundary layer are examined, and additional analytical and experimental results are presented. The probable ranges of pressure rises and flow deflections associated with separation are indicated. Consideration is given to the effects of Mach number, adverse pressure gradient, and Reynolds number for laminar boundary layers and to the effects of Mach number, Reynolds number, and ratio of sepcific heats for turbulent boundary layers.
Author | : |
Publisher | : |
Total Pages | : 0 |
Release | : 1967 |
Genre | : |
ISBN | : |
Download Effects of Initial Turbulent Boundary Layer on Shock-induced Separation in Transonic Flow Book in PDF, Epub and Kindle
Author | : International Union of Theoretical and Applied Mechanics |
Publisher | : |
Total Pages | : 432 |
Release | : 1958 |
Genre | : Aerodynamics |
ISBN | : |
Download Boundary Layer Research Book in PDF, Epub and Kindle
Author | : Piotr Doerffer |
Publisher | : Springer Science & Business Media |
Total Pages | : 350 |
Release | : 2010-11-25 |
Genre | : Technology & Engineering |
ISBN | : 3642030041 |
Download Unsteady Effects of Shock Wave induced Separation Book in PDF, Epub and Kindle
This volume contains description of experimental and numerical results obtained in the UFAST project. The goal of the project was to generate experiment data bank providing unsteady characteristics of the shock boundary layer interaction. The experiments concerned basic-reference cases and the cases with application of flow control devices. Obtained new data bank have been used for the comparison with available simulation techniques, starting from RANS, through URANS, LES and hybrid RANS-LES methods. New understanding of flow physics as well as ability of different numerical methods in the prediction of such unsteady flow phenomena will be discussed.