ADIGMA - A European Initiative on the Development of Adaptive Higher-Order Variational Methods for Aerospace Applications

Results of a collaborative research project funded by the European Union, 2006-2009

  • Norbert Kroll
  • Heribert Bieler
  • Herman Deconinck
  • Vincent Couaillier
  • Harmen van der Ven
  • Kaare Sørensen
Part of the Notes on Numerical Fluid Mechanics and Multidisciplinary Design book series (NNFM, volume 113)

Table of contents

  1. Front Matter
  2. The ADIGMA Project

    1. Norbert Kroll
      Pages 1-9
  3. Research Activities

    1. II.1 Higher-Order Discretization Methods

      1. F. Bassi, L. Botti, A. Colombo, A. Crivellini, N. Franchina, A. Ghidoni et al.
        Pages 25-38
      2. Arne Taube, Gregor Gassner, Claus-Dieter Munz
        Pages 53-65
      3. Jianxian Qiu, Jun Zhu
        Pages 67-80
      4. Vít Dolejší, Martin Holík, Jiří Hozman
        Pages 81-93
      5. R. Abgrall, A Larat, M. Ricchiuto
        Pages 107-128
      6. N. Villedieu, T. Quintino, M. Vymazal, H. Deconinck
        Pages 129-143
      7. Frédéric Chalot, Pierre-Elie Normand
        Pages 145-165
      8. Xi Du, Christophe Corre, Alain Lerat
        Pages 167-180
      9. Arne Taube, Claus-Dieter Munz
        Pages 195-207
    2. II.2 Solution Strategies

      1. R. Abgrall, R. Butel, P. Jacq, C. Lachat, X. Lacoste, A. Larat et al.
        Pages 209-224
      2. V. Couaillier, F. Renac, M. C. Le Pape
        Pages 225-242

About these proceedings

Introduction

This volume contains results gained from the EU-funded 6th Framework project ADIGMA (Adaptive Higher-order Variational Methods for Aerodynamic Applications in Industry). The goal of ADIGMA was the development and utilization of innovative adaptive higher-order methods for the compressible flow equations enabling reliable, mesh independent numerical solutions for large-scale aerodynamic applications in aircraft industry. The ADIGMA consortium was comprised of 22 organizations which included the main European aircraft manufacturers, the major European research establishments and several universities, all with well proven expertise in Computational Fluid Dynamics (CFD). The book presents an introduction to the project, exhibits partners’ methods and ap-proaches and provides a critical assessment of the newly developed methods for industrial aerodynamic applications. The best numerical strategies for integration as major building blocks for the next generation of industrial flow solvers are identified.

Keywords

Computational Fluid Dynamics (CFD) algorithms discontinuous Galerkin methods error estimation and local mesh higher-order solvers for Navier-Stokes equations multidimensional upwinding optimization p- and h- multigrid residual distribution schemes shock capturing methods

Editors and affiliations

  • Norbert Kroll
    • 1
  • Heribert Bieler
    • 2
  • Herman Deconinck
    • 3
  • Vincent Couaillier
    • 4
  • Harmen van der Ven
    • 5
  • Kaare Sørensen
    • 6
  1. 1.German Aerospace Center (DLR)BraunschweigGermany
  2. 2.Airbus Deutschland GmbHBremenGermany
  3. 3.von Karman Institute for Fluid Dynamics (VKI)Rhode-St-GeneseBelgium
  4. 4.ONERAChâtillonFrance
  5. 5.NLRAmsterdamThe Netherlands
  6. 6.EADS DeutschlandManchingGermany

Bibliographic information

  • DOI https://doi.org/10.1007/978-3-642-03707-8
  • Copyright Information Springer-Verlag Berlin Heidelberg 2010
  • Publisher Name Springer, Berlin, Heidelberg
  • eBook Packages Engineering
  • Print ISBN 978-3-642-03706-1
  • Online ISBN 978-3-642-03707-8
  • Series Print ISSN 1612-2909
  • Series Online ISSN 1060-0824