Author: Hans Wolfgang Liepmann
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 92
Book Description
Investigations of the Interaction of Boundary Layer and Shock Waves in Transonic Flow
Author: Hans Wolfgang Liepmann
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 92
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 92
Book Description
Shock Wave-Boundary-Layer Interactions
Author: Holger Babinsky
Publisher: Cambridge University Press
ISBN: 1139498649
Category : Technology & Engineering
Languages : en
Pages : 481
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.
Publisher: Cambridge University Press
ISBN: 1139498649
Category : Technology & Engineering
Languages : en
Pages : 481
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.
Investigations of the Interaction of Boundary Layer and Shock Waves in Transonic Flow
Author: Hans Wolfgang Liepmann
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 182
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 182
Book Description
Investigations of the Interaction Between Shock Waves and Boundary Layer in Transonic Flow
Author: H. W. Liepmann
Publisher:
ISBN:
Category :
Languages : en
Pages : 12
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 12
Book Description
Investigation of the Interaction of Boundary Layer and Shock Waves in Transonic Flow
Author: Hans Wolfgang Liepmann
Publisher:
ISBN:
Category :
Languages : en
Pages : 33
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 33
Book Description
Analytic Investigation of Transonic Normal Shock-Boundary Layer Interaction
Author: W. H. Mason
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 275
Book Description
Advances in inviscid transonic flow field computational capability and supercritical airfoil design make it important to understand of the the physics of normal shock-boundary layer interactions. In this work, the Navier-Stokes equations are thoroughly investigated through the use of perturbation methods and a generalized multi-region model is proposed for interactions between weak normal shock waves and turbulent boundary layers. This model is first applied to a highly idealized case in which a uniform subsonic flow is used to model the boundary layer, and analytic results for the wall and interface pressure are obtained.
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 275
Book Description
Advances in inviscid transonic flow field computational capability and supercritical airfoil design make it important to understand of the the physics of normal shock-boundary layer interactions. In this work, the Navier-Stokes equations are thoroughly investigated through the use of perturbation methods and a generalized multi-region model is proposed for interactions between weak normal shock waves and turbulent boundary layers. This model is first applied to a highly idealized case in which a uniform subsonic flow is used to model the boundary layer, and analytic results for the wall and interface pressure are obtained.
Investigation of Laminar and Turbulent Boundary Layers Interacting with Externally Generated Shock Waves
Author: Earl C. Watson
Publisher:
ISBN:
Category : Laminar boundary layer
Languages : en
Pages : 140
Book Description
Laminar and turbulent boundary layer interactions with externally generated shock waves.
Publisher:
ISBN:
Category : Laminar boundary layer
Languages : en
Pages : 140
Book Description
Laminar and turbulent boundary layer interactions with externally generated shock waves.
Physical Study of Shock-wave/boundary-layer Interaction Control in Transonic Flow
Author: Reynald Bur
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
A Theoretical Investigation of the Interaction Between Shock Waves and Unseparated Boundary Layers in Transonic Flow
Author: Howard Michael Brilliant
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 386
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 386
Book Description
An Experimental Investigation of Shock Wave -- Boundary Layer Interaction Dynamics
Author: Gerald W. Braun
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 254
Book Description
Wind tunnel tests were performed which simulated the flow pulsations which are sometimes produced in engine inlets by shock-boundary layer interaction. Shock Mach numbers from 1.2 to 1.4 were used and the boundary layer was influenced by air bleeding in or sucking off. The flow was observed by shodowgraph and static and total pressures were measured by means of low frequency and high frequency response instruments. Static wall pressures, boundary layer pressure profiles, and total pressure distributions across several tunnel cross sections were plotted. The data were analyzed with respect to their rms value and power spectral density. A literature survey and an analytical investigation of the pulsations in a diffuser with nonviscous flow are included. (Author).
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 254
Book Description
Wind tunnel tests were performed which simulated the flow pulsations which are sometimes produced in engine inlets by shock-boundary layer interaction. Shock Mach numbers from 1.2 to 1.4 were used and the boundary layer was influenced by air bleeding in or sucking off. The flow was observed by shodowgraph and static and total pressures were measured by means of low frequency and high frequency response instruments. Static wall pressures, boundary layer pressure profiles, and total pressure distributions across several tunnel cross sections were plotted. The data were analyzed with respect to their rms value and power spectral density. A literature survey and an analytical investigation of the pulsations in a diffuser with nonviscous flow are included. (Author).