Skip to main content
  • Conference proceedings
  • © 2010

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

  • State-of-the-art of the Development of Adaptive Higher-Order Variational Methods for Aerospace Applications
  • Contains the Results of a collaborative research project funded by the European Union, 2006-2009

Part of the book series: Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM, volume 113)

Buy it now

Buying options

eBook USD 259.00
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
Softcover Book USD 329.99
Price excludes VAT (USA)
  • Compact, lightweight edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info
Hardcover Book USD 329.99
Price excludes VAT (USA)
  • Durable hardcover edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info

Tax calculation will be finalised at checkout

Other ways to access

This is a preview of subscription content, log in via an institution to check for access.

Table of contents (34 papers)

  1. Front Matter

  2. The ADIGMA Project

    1. The ADIGMA Project

      • Norbert Kroll
      Pages 1-9
  3. Research Activities

    1. II.1 Higher-Order Discretization Methods

      1. Very High-Order Accurate Discontinuous Galerkin Computation of Transonic Turbulent Flows on Aeronautical Configurations
        • F. Bassi, L. Botti, A. Colombo, A. Crivellini, N. Franchina, A. Ghidoni et al.
        Pages 25-38
      2. Explicit One-Step Discontinuous Galerkin Schemes for Unsteady Flow Simulations
        • Arne Taube, Gregor Gassner, Claus-Dieter Munz
        Pages 53-65
      3. RKDG with WENO Type Limiters
        • Jianxian Qiu, Jun Zhu
        Pages 67-80
      4. IPG Discretizations of the Compressible Navier-Stokes Equations
        • Vít Dolejší, Martin Holík, Jiří Hozman
        Pages 81-93
      5. Construction of High-Order Non Upwind Distribution Schemes
        • R. Abgrall, A Larat, M. Ricchiuto
        Pages 107-128
      6. High Order Residual Distribution Schemes Based on Multidimensional Upwinding
        • N. Villedieu, T. Quintino, M. Vymazal, H. Deconinck
        Pages 129-143
      7. Higher-Order Stabilized Finite Elements in an Industrial Navier-Stokes Code
        • Frédéric Chalot, Pierre-Elie Normand
        Pages 145-165
      8. A Third-Order Finite-Volume Residual-Based Scheme on Unstructured Grids
        • Xi Du, Christophe Corre, Alain Lerat
        Pages 167-180
      9. Synthesis Report on Shock Capturing Strategies
        • Arne Taube, Claus-Dieter Munz
        Pages 195-207
    2. II.2 Solution Strategies

      1. Implicit Strategy and Parallelization of a High Order Residual Distribution Scheme
        • R. Abgrall, R. Butel, P. Jacq, C. Lachat, X. Lacoste, A. Larat et al.
        Pages 209-224
      2. Hybrid Multigrid DG/FV Methods for Viscous Turbulent Flows
        • V. Couaillier, F. Renac, M. C. Le Pape
        Pages 225-242

About this book

<P>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 approaches 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. </P>

Editors and Affiliations

  • German Aerospace Center (DLR), Braunschweig, Germany

    Norbert Kroll

  • Airbus Deutschland GmbH, Bremen, Germany

    Heribert Bieler

  • von Karman Institute for Fluid Dynamics (VKI), Rhode-St-Genese, Belgium

    Herman Deconinck

  • ONERA, Châtillon, France

    Vincent Couaillier

  • NLR, Amsterdam, The Netherlands

    Harmen Ven

  • EADS Deutschland, Manching, Germany

    Kaare Sørensen

Bibliographic Information

Buy it now

Buying options

eBook USD 259.00
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
Softcover Book USD 329.99
Price excludes VAT (USA)
  • Compact, lightweight edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info
Hardcover Book USD 329.99
Price excludes VAT (USA)
  • Durable hardcover edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info

Tax calculation will be finalised at checkout

Other ways to access