An adjoint-truncation error based approach for goal-oriented mesh adaptation
IMPLEMENTATION OF AN ADJOINT-BASED ERROR ESTIMATION AND GRID ADAPTATION MODULE IN THE DLR TAU CODE
Automatic Transition Prediction for RANS Computations Applied to a Generic High-Lift Wing AIAA Paper
Improved CFD Predictions for High Lift Flows in the European Project EUROLIFT II
Comparison of Mesh Adaptation Using the Adjoint Methodology and Truncation Error Estimates
An interpolation tool for aerodynamic mesh deformation problems based on octree decomposition