NASA NTRS · 20040152047
AIC Computations Using Navier-Stokes Equations on Single Image Supercomputers For Design Optimization
Abstract
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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Guruswamy, Guru. 2004-07-27. AIC Computations Using Navier-Stokes Equations on Single Image Supercomputers For Design Optimization. https://ntrs.nasa.gov/citations/20040152047
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