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Aerodynamic design optimization of nacelle/pylon position on an aircraft 被引量:10
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作者 Li Jing Gao Zhenghong +1 位作者 Huang Jiangtao Zhao Ke 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2013年第4期850-857,共8页
The arbitrary space-shape free form deformation (FFD) method developed in this paper is based on non-uniform rational B-splines (NURBS) basis function and used for the integral parameterization of nacelle-pylon ge... The arbitrary space-shape free form deformation (FFD) method developed in this paper is based on non-uniform rational B-splines (NURBS) basis function and used for the integral parameterization of nacelle-pylon geometry. The multi-block structured grid deformation technique is established by Delaunay graph mapping method. The optimization objects of aerodynamic characteristics are evaluated by solving NavierStokes equations on the basis of multi-block structured grid. The advanced particle swarm optimization (PSO) is utilized as search algorithm, which com-bines the Kriging model as surrogate model during optimization. The optimization system is used for optimizing the nacelle location of DLR-F6 wing-body-pylon-nacelle. The results indicate that the aerodynamic interference between the parts is significantly reduced. The optimization design system established in this paper has extensive applications and engineering value. 展开更多
关键词 delaunay graph mapping free form deformation (ffd kriging model navier-stokes equations particle swarm optimization (pso space-shape
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