DLR-F6 Wing Body configuration is a representative of a modern, twin-engine, transport aircraft configuration designed to fly at transonic speed. This configuration was used for analyzing state-of-the-art CFD technology in second AIAA drag prediction workshop. In this study, computations are performed for steady, transonic and turbulent flow past DLR wing-body configuration.
(Our sincere thanks to the CFD and HPC team at CRL, Pune ( http://crlindia.com ) for enabling us in generating the parallel data.)
