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Unsteady Effects of Shock Wave induced Separation

  • Conference proceedings
  • © 2011

Overview

  • Control of shock related unsteadiness.
  • Written by leading experts in this field
  • State-of-the-Art book

Part of the book series: Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM, volume 114)

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Table of contents (14 papers)

  1. Introduction — UFAST Project Overview

  2. Part I Transonic Interactions

  3. Part II Nozzle Flows

  4. Part III Shock Reflection

  5. Part IV Summary by Work Packages

About this book

This volume contains description of experimental and numerical results obtained in the UFAST project. The goal of the project was to generate experiment data bank providing unsteady characteristics of the shock boundary layer interaction. The experiments concerned basic-reference cases and the cases with application of flow control devices. Obtained new data bank have been used for the comparison with available simulation techniques, starting from RANS, through URANS, LES and hybrid RANS-LES methods. New understanding of flow physics as well as ability of different numerical methods in the prediction of such unsteady flow phenomena will be discussed.

Authors and Affiliations

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

    Piotr Doerffer

  • Numerical Mechanics Application, International, Brussels, Belgium

    Charles Hirsch

  • Directeur de Recherche au CNRS, IUSTI, Supersonic Group, Marseille Cedex 13, France

    Jean-Paul Dussauge

  • Engineering Department, University of Cambridge, Cambridge, United Kingdom

    Holger Babinsky

  • CFD Laboratory, Department of Engineering, The University of Liverpool, Liverpool, United Kingdom

    George N. Barakos

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