Parallel adjoint-based optimisation of a blended wing body aircraft with shock control bumps
作者： W. S. Wong , A. Le Moigne , N. Qin
DOI: 10.1017/S0001924000004425
关键词: Grid 、 Wingtip device 、 Sensitivity (control systems) 、 Solver 、 Control theory 、 Aerodynamics 、 Airfoil 、 Shock (mechanics) 、 Engineering 、 Wing
摘要: … out by employing an efficient adjoint-based … the adjoint solver have to be parallelised with a good parallel efficiency. This paper reports the parallel implementation efforts on the adjoint …
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