Computations from the Fourth Drag Prediction Workshop Using the Edge Solver
Drag Prediction for the DLR-F6 Wing-Body Configuration Using the Edge Solver
Results from the Second AIAA CFD High-Lift Prediction Workshop Using Edge
IMPROVING STALL CHARACTERISTICS OF UCAV WING WITH VORTEX GENERATORS
Numerical Validation of a Half Model High Lift Configuration in a Wind Tunnel AIAA Paper
Results from the 2^n^d AIAA CFD High Lift Prediction Workshop using Edge (AIAA 2014-0750)
Some Modeling Aspects in Computations of Turbulent Flow around High-Lift Configuration
Virtual Aircraft Design and Control of TransCruiser - A Canard Configuration
Drag Prediction for the DLR-F6 Wing-Body Configuration Using the Edge Solver AIAA Paper
IMPROVING THE PREDICTION FOR THE NASA HIGH-LIFT TRAP WING MODEL
Computations from the 4th Drag Prediction Workshop Using the Edge Solver
Integration of Thermal-Structural Analysis in the Product Development Process