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Notes on Numerical Fluid Mechanics and Multidisciplinary Design

Transition Location Effect on Shock Wave Boundary Layer Interaction

Experimental and Numerical Findings from the TFAST Project

Editors: Doerffer, P., Flaszynski, P., Dussauge, J.-P., Babinsky, H., Grothe, P., Petersen, A., Billard, F. (Eds.)

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  • Presents advanced methods for improving flow performance
  • Fosters a better understanding the consequences of laminar interactions
  • Shows how CFD can be used to predict complex flow phenomena
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  • ISBN 978-3-030-47461-4
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About this book

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.

Table of contents (7 chapters)

Table of contents (7 chapters)

Buy this book

eBook $149.00
price for Mexico
  • ISBN 978-3-030-47461-4
  • Digitally watermarked, DRM-free
  • Included format: PDF, EPUB
  • ebooks can be used on all reading devices
  • Immediate eBook download after purchase
Hardcover $199.99
price for Mexico
  • ISBN 978-3-030-47460-7
  • Free shipping for individuals worldwide
  • Immediate ebook access, if available*, with your print order
  • Usually dispatched within 3 to 5 business days.
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Bibliographic Information

Bibliographic Information
Book Title
Transition Location Effect on Shock Wave Boundary Layer Interaction
Book Subtitle
Experimental and Numerical Findings from the TFAST Project
Editors
  • Piotr Doerffer
  • Pawel Flaszynski
  • Jean-Paul Dussauge
  • Holger Babinsky
  • Patrick Grothe
  • Anna Petersen
  • Flavien Billard
Series Title
Notes on Numerical Fluid Mechanics and Multidisciplinary Design
Series Volume
144
Copyright
2021
Publisher
Springer International Publishing
Copyright Holder
Springer Nature Switzerland AG
eBook ISBN
978-3-030-47461-4
DOI
10.1007/978-3-030-47461-4
Hardcover ISBN
978-3-030-47460-7
Series ISSN
1612-2909
Edition Number
1
Number of Pages
VIII, 540
Number of Illustrations
94 b/w illustrations, 424 illustrations in colour
Topics

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