Transition Location Effect on Shock Wave Boundary Layer Interaction

Name: Transition Location Effect on Shock Wave Boundary Layer Interaction
Brand: Springer Nature Switzerland AG
SKU: 9783030474607
Price: 157.37 EUR
Availability: InStock

Experimental and Numerical Findings from the TFAST Project

Автор: Piotr Doerffer, Pawel Flaszynski, Jean-Paul Dussauge, Holger Babinsky, Patrick Grothe, Anna Petersen, Flavien Billard

Език:

Корици: С твърди корици

Издател: Springer Nature Switzerland AG

Наличност: Външен склад

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157.37 € 307.80 лв

This book presents experimental and numerical findings on reducing shock-induced separation by apply...

Информация за книгата

Автор

Piotr Doerffer, Pawel Flaszynski, Jean-Paul Dussauge, Holger Babinsky, Patrick Grothe, Anna Petersen, Flavien Billard

Език

Английски език

Корици

Книга - С твърди корици

Издадена

2020

страници

540

EAN

9783030474607

Enbook ID

28700631

Издател

Springer Nature Switzerland AG

Теглоt

980

Размери

155 x 235 x 35

Пълно описание

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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Transition Location Effect on Shock Wave Boundary Layer Interaction

Experimental and Numerical Findings from the TFAST Project

Информация за книгата

Пълно описание

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