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AIC Computations Using Navier-Stokes Equations on Single Image Supercomputers For Design Optimization

机译:在单幅超级计算机上使用Navier-stokes方程进行设计优化的aIC计算

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A procedure to accurately generate AIC using the Navier-Stokes solver including grid deformation is presented. Preliminary results show good comparisons between experiment and computed flutter boundaries for a rectangular wing. A full wing body configuration of an orbital space plane is selected for demonstration on a large number of processors. In the final paper the AIC of full wing body configuration will be computed. The scalability of the procedure on supercomputer will be demonstrated.

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