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4th International Workshop on High-Order CFD Methods
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  • Test cases
    • Baseline test cases
      • BI1 - Inviscid vortex transport
      • BI2 - Inviscid flow over a bump
      • BI3 - Inviscid bow shock
      • BL1 - Laminar Joukowski airfoil, Re=1000
      • BL2 - Laminar shock-boundary layer interaction
      • BL3 - Heaving & pitching airfoil
      • BR1 - RANS of Joukowski airfoil
      • BS1 - Taylor-Green vortex, Re=1600
      • BS2 - LES channel flow Ret=590
    • Advanced test cases
      • AR1 - Common Research Model (Drag Prediction Workshop 5)
      • AR2 - RANS of the transonic turbulent flow in a 3D channel with a swept bump
      • AS1 - DNS/LES of the infinite cylinder at Re=3900
      • AS2 - Spanwise periodic DNS/LES of transitional turbine cascades
    • Computional/meshing challenges
      • C1 - DLR F11
      • C2 - NASA Rotor 67
  • Guidelines
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    • Advanced and complex test cases
    • Baseline test case summaries
    • Code presentations
    • MS910 at Eccomas CFD 2016_old
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  • Previous
    • HOW1 - 50th AIAA Aerospace Sciences Meeting, Nashville, 7-8 January 2012
    • HOW2 - Cologne, 27-28 May 2013
    • HOW3 - 53rd AIAA Aerospace Sciences Meeting, Kissimee, 3-4 January 2015
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Home»Previous editions

Previous editions

1st International Workshop on High-Order CFD Methods

2nd International Workshop on High-Order CFD Methods

3rd International Workshop on High-Order CFD Methods

News

  • BL2 - Laminar shock boundary interaction : description corrected
  • BL3 - important change in the test case description
  • AS1 - Update of the test case description
  • Abstract submission for the minisymposium at Eccomas
  • Update of the AS2 test case - Spanwise periodic DNS/LES of transitional turbine cascades
  • Update of the AR1 and AS1 test cases
  • Update of test case BL3 - Heaving and pitching airfoil

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