Investigation of Laminar and Turbulent Boundary Layers Interacting with Externally Generated Shock Waves PDF Download
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Author: Earl C. Watson
Publisher:
ISBN:
Category : Laminar boundary layer
Languages : en
Pages : 140
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Book Description
Laminar and turbulent boundary layer interactions with externally generated shock waves.
Author: Earl C. Watson
Publisher:
ISBN:
Category : Laminar boundary layer
Languages : en
Pages : 140
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Book Description
Laminar and turbulent boundary layer interactions with externally generated shock waves.
Author: Earl C. Watson
Publisher:
ISBN:
Category : Laminar flow
Languages : en
Pages : 0
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Book Description
Author: Holger Babinsky
Publisher: Cambridge University Press
ISBN: 1139498649
Category : Technology & Engineering
Languages : en
Pages : 481
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Book Description
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: William C. Rose
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 28
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Book Description
Method for predicting interaction produced by externally generated, oblique shock wave impinging on laminar or turbulent boundary layers.
Author: International Union of Theoretical and Applied Mechanics
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 432
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Book Description
Author: William Russell Seebaugh
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 920
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Book Description
Author: C. C. Sun
Publisher:
ISBN:
Category : Shock waves
Languages : en
Pages : 916
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Book Description
Tabulated data from a series of experimental studies of the interaction of a shock wave with a turbulent boundary layer in axisymmetric flow configurations is presented. The studies were conducted at the walls of circular wind tunnels and on the cylindrical centerbody of an annular flow channel. Detailed pitot pressure profiles and wall static pressure profiles upstream of, within and downstream of the interaction region are given. Results are presented for flows at nominal freestream Mach Numbers of 2, 3 and 4. For studies at the tunnel sidewalls, the shock waves were produced by conical shock generators mounted on the centerline of the wind tunnel at zero angle of attack. The annular ring generator was used to produce the shock wave at the centerbody of the annular flow channel. The effects of boundary layer bleed were examined in the investigation. Both bleed rate and bleed location were studied. Most of the bleed studies were conducted with bleed holes drilled normal to the wall surface but the effects of slot suction were also examined. A summary of the principal results and conclusions is given.
Author: Neale A. Messina
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 386
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Book Description
Author: Raymond L. Chuan
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 114
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Book Description
Author: W W Koepcke
Publisher: Hassell Street Press
ISBN: 9781019363461
Category :
Languages : en
Pages : 0
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Book Description
This book is a scientific investigation into the interaction between laminar boundary layers and shock waves, with a focus on the separation of flow. Written by W. W. Koepcke, it is a detailed study of the phenomenon and its practical implications. The book contains a wealth of data and analysis, making it a valuable reference for researchers, engineers, and students in the field of fluid dynamics. This work has been selected by scholars as being culturally important, and is part of the knowledge base of civilization as we know it. This work is in the "public domain in the United States of America, and possibly other nations. Within the United States, you may freely copy and distribute this work, as no entity (individual or corporate) has a copyright on the body of the work. Scholars believe, and we concur, that this work is important enough to be preserved, reproduced, and made generally available to the public. We appreciate your support of the preservation process, and thank you for being an important part of keeping this knowledge alive and relevant.
