From a05dd8cd2f508387124c087e8e7b208dfe49f831 Mon Sep 17 00:00:00 2001 From: hartmann Date: Tue, 7 Aug 2012 11:00:51 +0000 Subject: [PATCH] Update refs. git-svn-id: https://svn.dealii.org/trunk@25754 0785d39b-7218-0410-832d-ea1e28bc413d --- deal.II/doc/publications/index.html | 96 ++++++++++++++++++----------- 1 file changed, 59 insertions(+), 37 deletions(-) diff --git a/deal.II/doc/publications/index.html b/deal.II/doc/publications/index.html index 0cf3ba5081..e10389e24a 100644 --- a/deal.II/doc/publications/index.html +++ b/deal.II/doc/publications/index.html @@ -393,6 +393,32 @@ Preprint, University of Heidelberg, Germany, 2011. +
  • + R. Hartmann +
    + Higher-order and adaptive discontinuous Galerkin + methods with shock-capturing applied to transonic turbulent + delta wing flow + +
    + 50th AIAA Aerospace Sciences Meeting, AIAA 2012-459, 2012. +
    • + +
  • + R. Hartmann +
    + Higher-order and adaptive Discontinuous Galerkin + methods applied to turbulent delta wing flow +
    + In H. P. Kreplin, editor, New Results in Numerical and + Experimental Fluid Mechanics VIII: Contributions to the 17th + STAB/DGLR Symposium Berlin, Germany, 2010, Notes on + Numerical Fluid Mechanics and Multidisciplinary Design, + Springer. In press. +
    • +
  • T. Heister, G. Rapin
    Efficient augmented Lagrangian-type preconditioning @@ -542,6 +568,23 @@ pp. 3186-3197, 2012.
    • +
  • M. Wallraff, T. Leicht, M. Lange-Hegermann +
    + Numerical flux functions for Reynolds-averaged Navier-Stokes + and kω turbulence model computations with a line-preconditioned + p-multigrid discontinuous Galerkin solver +
    + Int. J. Numer. Meth. Fluids, published online, 2012. +
    • + +
  • M. Wallraff, T. Leicht, M. Lange-Hegermann +
    + Numerical flux functions for RANS-kω computations with a + line-implicit p-multigrid DG solver +
    + 50th AIAA Aerospace Sciences Meeting, AIAA 2012-458, 2012. +
    • +
  • J. Willems
    Robust Multilevel Methods for General Symmetric Positive Definite Operators @@ -732,30 +775,6 @@ SIAM J. of Numerical Analysis, vol. 49, pp. 917-944, 2011.
    • -
  • R. Hartmann -
    - Higher-order and adaptive Discontinuous Galerkin - methods applied to turbulent delta wing flow -
    - In H. P. Kreplin, editor, New Results in Numerical and - Experimental Fluid Mechanics VIII: Contributions to the 17th - STAB/DGLR Symposium Berlin, Germany, 2010, Notes on - Numerical Fluid Mechanics and Multidisciplinary Design, - Springer. To appear. -
    • - -
  • - R. Hartmann -
    - Higher-order and adaptive discontinuous Galerkin - methods with shock-capturing applied to transonic turbulent - delta wing flow - -
    - 50thAIAA Aerospace Sciences Meeting, 2012. Submitted. -
    • -
  • R. Hartmann, J. Held, T. Leicht
    @@ -766,18 +785,6 @@ J. Comput. Phys., vol. 230, pp. 4268-4284, 2011.
    • -
  • R. Hartmann, J. Held, T. Leicht, F. Prill -
    - Error estimation and adaptive mesh refinement for aerodynamic flows - -
    - In N. Kroll, H. Bieler, H. Deconinck, V. Couallier, H. van der Ven and K. Sorensen, editors, - ADIGMA - A European Initiative on the Development of Adaptive - Higher-Order Variational Methods for Aerospace Applications, - Springer, to appear, 2010. -
    • -
  • T. Heister
    A Massively Parallel Finite Element Framework with @@ -918,7 +925,7 @@ refinement for aerodynamic flows.
    - 49th49th AIAA Aerospace Sciences Meeting, 2011. + 49th AIAA Aerospace Sciences Meeting AIAA 2011-212, 2011.
  • @@ -1384,6 +1391,21 @@ Aerospace Science and Technology, vol. 14, pp. 512-529, 2010.
    • +
  • R. Hartmann, J. Held, T. Leicht, F. Prill +
    + Error estimation and adaptive mesh refinement for aerodynamic flows + +
    + In N. Kroll, H. Bieler, H. Deconinck, V. Couallier, H. van der Ven + and K. Sorensen, editors, ADIGMA - A European Initiative on the + Development of Adaptive Higher-Order Variational Methods for + Aerospace Applications, +
    + vol. 113 of Notes on numerical fluid mechanics and + multidisciplinary design, pp. 339-353, Springer, 2010. +
    • +
  • R. Hartmann, P. Houston
    -- 2.39.5