Overview
- 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
Part of the book series: Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM, volume 144)
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Table of contents (7 chapters)
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Front Matter
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Basic Flow Cases
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Front Matter
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Application Flow Cases
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Front Matter
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Summary, Conclusions and Lessons Learned
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Front Matter
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Keywords
- Laminar and Turbulent Boundary Layer
- Shock Induced Separation
- Transition Location Effect
- Models of Flow Control Devices
- Simulations of 3-D transonic Wing
- Hybrid RANS-LENS Methods
- URANS Methods
- Reduce Flow Separation
- Compressible Flows
- Induced Transition to Turbulence
- Transonic Turbine Flow
- Transonic Wing Flow
- Compressor and Fan Blade Aerodynamics
- High Pressure Turbine Blade
- TFAST Project
- fluid- and aerodynamics
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.
Editors and Affiliations
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
DOI: https://doi.org/10.1007/978-3-030-47461-4
Publisher: Springer Cham
eBook Packages: Engineering, Engineering (R0)
Copyright Information: Springer Nature Switzerland AG 2021
Hardcover ISBN: 978-3-030-47460-7Published: 31 July 2020
Softcover ISBN: 978-3-030-47463-8Published: 01 August 2021
eBook ISBN: 978-3-030-47461-4Published: 30 July 2020
Series ISSN: 1612-2909
Series E-ISSN: 1860-0824
Edition Number: 1
Number of Pages: VIII, 540
Number of Illustrations: 94 b/w illustrations, 424 illustrations in colour
Topics: Engineering Fluid Dynamics, Fluid- and Aerodynamics, Engine Technology, Engineering Thermodynamics, Heat and Mass Transfer