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Towards an efficient and robust numerical strategy for fast aerodynamic performance prediction on launch vehicles
2017
The present work aims at increasing the responsiveness of aerodynamic coefficient predictions for the investigation of the effects of technological details. Starting from a simplified configuration and using Zonal Immersed Boundary Conditions which combine the local use of both a modelling method (e.g. RANS, URANS, ZDES, LES or DNS) and IBC (Immersed Boundary Conditions), realistic configurations are rapidly turned into feasible numerical simulations. In this paper, the efficiency and the
doi:10.13009/eucass2017-496
fatcat:w5szunaus5gnzpvh4yzpgtbaea