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  • Open Daily: 10am - 10pm
    Alley-side Pickup: 10am - 7pm

    3038 Hennepin Ave Minneapolis, MN
    612-822-4611

Open Daily: 10am - 10pm | Alley-side Pickup: 10am - 7pm
3038 Hennepin Ave Minneapolis, MN
612-822-4611
Transition Location Effect on Shock Wave Boundary Layer Interaction: Experimental and Numerical Findings from the Tfast Project

Transition Location Effect on Shock Wave Boundary Layer Interaction: Experimental and Numerical Findings from the Tfast Project

Doerffer, Piotr
Flaszynski, Pawel
Dussauge, Jean-Paul

Paperback

Series: Notes on Numerical Fluid Mechanics and Multidisciplinary Des, Book 144

Technology & EngineeringPhysics

ISBN10: 3030474631
ISBN13: 9783030474638
Publisher: Springer Nature
Published: Aug 1 2021
Pages: 540
Weight: 1.68
Height: 1.11 Width: 6.14 Depth: 9.21
Language: English

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.

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