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    • Time-resolved adaptive FEM simulation of the DLR-F11 aircraft model at high Reynolds number 

      Hoffman J.; Jansson J.; Jansson N.; de Abreu R.V. (52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014, 2014-12-31)
      We present a time-resolved, adaptive finite element method for aerodynamics, together with the results from the HiLiftPW-2 workshop, where this method is used to compute the ow past a DLR-F11 aircraft model at realistic ...