Transition Location Effect on Shock Wave Boundary Layer Interaction

1. Front Matter

   Pages i-viii

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2. Introduction—TFAST Overview

   • Piotr Doerffer

   Pages 1-21

3. Basic Flow Cases

   1. Front Matter

      Pages 23-23

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   2. WP-1 Reference Cases of Laminar and Turbulent Interactions

      • Jean-Paul Dussauge, Reynald Bur, Todd Davidson, Holger Babinsky, Matteo Bernardini, Sergio Pirozzoli et al.

      Pages 25-127

   3. WP-2 Basic Investigation of Transition Effect

      • Holger Babinsky, Pierre Dupont, Pavel Polivanov, Andrey Sidorenko, Reynald Bur, Rogier Giepman et al.

      Pages 129-225

4. Application Flow Cases

   1. Front Matter

      Pages 227-227

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   2. WP-3 Internal Flows—Compressors

      • Patrick Grothe, Pawel Flaszynski, Ryszard Szwaba, Michal Piotrowicz, Piotr Kaczynski, Benoit Tartinville et al.

      Pages 229-296

   3. WP-4 Internal Flows—Turbine

      • Anna Petersen, Piotr Doerffer, Pawel Flaszynski, Ryszard Szwaba, Michal Piotrowicz, Piotr Kaczynski et al.

      Pages 297-346

   4. WP-5 External Flows—Wing

      • Flavien Billard, Todd Davidson, Holger Babinsky, Robert Placek, Marek Miller, Paweł Ruchała et al.

      Pages 347-512

5. Summary, Conclusions and Lessons Learned

   1. Front Matter

      Pages 513-513

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   2. Closing Remarks

      • Pawel Flaszynski, Piotr Doerffer, Sergio Pirozzoli, Jean-Paul Dussauge, Pierre Dupont, Lionel Larchevêque et al.

      Pages 515-540

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.

• 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

• Institute of Fluid Flow Machinery, Polish Academy of Sciences, IMP PAN, Gdansk, Poland

  Piotr Doerffer, Pawel Flaszynski

• Supersonic Group, IUSTI, Marseille, France

  Jean-Paul Dussauge

• Department of Engineering, University of Cambridge, Cambridge, UK

  Holger Babinsky

• Rolls-Royce Deutschland Ltd, Blankenfelde-Mahlow, Germany

  Patrick Grothe

• German Aerospace Center (DLR), Institute of Propulsion Technology, Göttingen, Germany

  Anna Petersen

• Aircraft Engineering and Loads Division, Dassault Aviation, Saint-Cloud, France

  Flavien Billard

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