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Transition Location Effect on Shock Wave Boundary Layer Interaction [electronic resource] : Experimental and Numerical Findings from the TFAST Project / edited by Piotr Doerffer, Pawel Flaszynski, Jean-Paul Dussauge, Holger Babinsky, Patrick Grothe, Anna Petersen, Flavien Billard.

Contributor(s): Doerffer, Piotr [editor.] | Flaszynski, Pawel [editor.] | Dussauge, Jean-Paul [editor.] | Babinsky, Holger [editor.] | Grothe, Patrick [editor.] | Petersen, Anna [editor.] | Billard, Flavien [editor.] | SpringerLink (Online service).
Material type: materialTypeLabelBookSeries: Notes on Numerical Fluid Mechanics and Multidisciplinary Design: 144Publisher: Cham : Springer International Publishing : Imprint: Springer, 2021Edition: 1st ed. 2021.Description: VIII, 540 p. 518 illus., 424 illus. in color. online resource.Content type: text Media type: computer Carrier type: online resourceISBN: 9783030474614.Subject(s): Fluid mechanics | Continuum mechanics | Engines | Thermodynamics | Heat engineering | Heat transfer | Mass transfer | Engineering Fluid Dynamics | Continuum Mechanics | Engine Technology | Engineering Thermodynamics, Heat and Mass TransferAdditional physical formats: Printed edition:: No title; Printed edition:: No title; Printed edition:: No titleDDC classification: 620.1064 Online resources: Click here to access online
Contents:
Introduction – TFAST Overview -- WP-1 Reference Cases of Laminar and Turbulent Interactions -- WP-2 Basic Investigation of Transition Effect -- WP-3 Internal Flows – Compressors -- WP-4 Internal Flows – Turbine -- WP-5 External Flows – Wing -- Closing Remarks.
In: Springer Nature eBookSummary: This book presents experimental and numerical findings on reducing shock-induced separation by applying transition upstream the shock wave. The purpose is to find out how close to the shock wave the transition should be located in order to obtain favorable turbulent boundary layer interaction. The book shares findings obtained using advanced flow measurement methods and concerning e.g. the transition location, boundary layer characteristics, and the detection of shock wave configurations. It includes a number of experimental case studies and CFD simulations that offer valuable insights into the flow structure. It covers RANS/URANS methods for the experimental test section design, as well as more advanced techniques, such as LES, hybrid methods and DNS for studying the transition and shock wave interaction in detail. The experimental and numerical investigations presented here were conducted by sixteen different partners in the context of the TFAST Project. The general focus is on determining if and how it is possible to improve flow performance in comparison to laminar interaction. The book mainly addresses academics and professionals whose work involves the aerodynamics of internal and external flows, as well as experimentalists working with compressible flows. It will also be of benefit for CFD developers and users, and for students of aviation and propulsion systems alike.
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Introduction – TFAST Overview -- WP-1 Reference Cases of Laminar and Turbulent Interactions -- WP-2 Basic Investigation of Transition Effect -- WP-3 Internal Flows – Compressors -- WP-4 Internal Flows – Turbine -- WP-5 External Flows – Wing -- Closing Remarks.

This book presents experimental and numerical findings on reducing shock-induced separation by applying transition upstream the shock wave. The purpose is to find out how close to the shock wave the transition should be located in order to obtain favorable turbulent boundary layer interaction. The book shares findings obtained using advanced flow measurement methods and concerning e.g. the transition location, boundary layer characteristics, and the detection of shock wave configurations. It includes a number of experimental case studies and CFD simulations that offer valuable insights into the flow structure. It covers RANS/URANS methods for the experimental test section design, as well as more advanced techniques, such as LES, hybrid methods and DNS for studying the transition and shock wave interaction in detail. The experimental and numerical investigations presented here were conducted by sixteen different partners in the context of the TFAST Project. The general focus is on determining if and how it is possible to improve flow performance in comparison to laminar interaction. The book mainly addresses academics and professionals whose work involves the aerodynamics of internal and external flows, as well as experimentalists working with compressible flows. It will also be of benefit for CFD developers and users, and for students of aviation and propulsion systems alike.

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