Multiblock Grid Generation

Results of the EC/BRITE-EURAM Project EUROMESH, 1990–1992

  • Editors
  • Nigel P. Weatherill
  • Michael J. Marchant
  • D. A. King

Part of the Notes on Numerical Fluid Mechanics (NNFM) book series (NNFM, volume 44)

Table of contents

  1. Front Matter
    Pages I-VIII
  2. Introduction

    1. Front Matter
      Pages 1-1
    2. D. A. King
      Pages 3-5
  3. Topology Generation

    1. Front Matter
      Pages 19-19
    2. V. Tréguer-Katossky, D. Bertin, E. Chaput
      Pages 21-26
    3. Riccardo Scateni
      Pages 27-31
  4. Surface Grid Generation and Geometry Modelling

    1. Front Matter
      Pages 35-35
    2. José M. de la Viuda
      Pages 37-44
    3. B. Morin, V. Tréguer-Katossky
      Pages 48-54
    4. Helmut Sobieczky
      Pages 71-76
  5. Volume Grid Generation

    1. Front Matter
      Pages 77-77
    2. José M. de la Viuda, Juan J. Guerra, A. Abbas
      Pages 79-85
    3. J. Oppelstrup, O. Runborg, P. Mineau, P. Weinerfelt, R. Lehtimäki, B. Arlinger
      Pages 117-129
    4. T. Fol, V. Tréguer-Katossky
      Pages 130-138

About this book

Introduction

Computational Fluid Dynamics research, especially for aeronautics, continues to be a rewarding and industrially relevant field of applied science in which to work. An enthusiastic international community of expert CFD workers continue to push forward the frontiers of knowledge in increasing number. Applications of CFD technology in many other sectors of industry are being successfully tackled. The aerospace industry has made significant investments and enjoys considerable benefits from the application of CFD to its products for the last two decades. This era began with the pioneering work ofMurman and others that took us into the transonic (potential flow) regime for the first time in the early 1970's. We have also seen momentous developments of the digital computer in this period into vector and parallel supercomputing. Very significant advances in all aspects of the methodology have been made to the point where we are on the threshold of calculating solutions for the Reynolds-averaged Navier-Stokes equations for complete aircraft configurations. However, significant problems and challenges remain in the areas of physical modelling, numerics and computing technology. The long term industrial requirements are captured in the U. S. Governments 'Grand Challenge' for 'Aerospace Vehicle Design' for the 1990's: 'Massively parallel computing systems and advanced parallel software technology and algorithms will enable the development and validation of multidisciplinary, coupled methods. These methods will allow the numerical simulation and design optimisation of complete aerospace vehicle systems throughout the flight envelope'.

Keywords

Reynolds-averaged Navier-Stokes computational fluid dynamics computer dynamics fluid dynamics

Bibliographic information

  • DOI https://doi.org/10.1007/978-3-322-87881-6
  • Copyright Information Springer Fachmedien 1993
  • Publisher Name Vieweg+Teubner Verlag
  • eBook Packages Springer Book Archive
  • Print ISBN 978-3-528-07644-3
  • Online ISBN 978-3-322-87881-6
  • Series Print ISSN 1612-2909
  • Series Online ISSN 1860-0824
  • About this book
Industry Sectors
Pharma
Automotive
Chemical Manufacturing
Biotechnology
Electronics
Consumer Packaged Goods
Energy, Utilities & Environment
Aerospace
Oil, Gas & Geosciences