| Document Date: 2006-04-24 01:05:54
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City Cambridge / Residual / / Company Ip / Reno NV / Astronautics Inc. / Intel / / / Facility American Institute of Aeronautics / / IndustryTerm multigrid algorithm / tridiagonal systems / pth order solution / coarse level solution / accuracy solutions / block-tridiagonal algorithm / aerospace design / convective systems / state prolongation operator / lower-order systems / iterative algorithm / fine level solution / line smoothing algorithm / line creation algorithm / aerospace vehicles / p-multigrid algorithm / residual restriction operator / final solution / state restriction operator / multigrid solution algorithms / prolongation operator / order solution / gas dynamics / iterative solution / finite-volume algorithms / transfer operators / line-creation algorithm / steady-state solution / iterative algorithms / finite volume algorithms / / Organization American Institute of Aeronautics / / Person David L. Darmofal / Forward Path / / / Position Research Assistant / Associate Professor / Senior Member AIAA / Mp / / Product MG iterations -2 / / ProgrammingLanguage E / / ProvinceOrState Massachusetts / / Technology line creation algorithm / block-tridiagonal algorithm / line block Jacobi algorithm / RAM / multigrid algorithm / 0436 Line Creation Algorithm / line-creation algorithm / p-multigrid algorithm / solution algorithm / multigrid solution algorithms / iterative algorithm / finite-volume algorithms / finite volume algorithms / line smoothing algorithm / /
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42nd AIAA Aerospace Sciences Meeting and Exhibit, Paper Number[removed]Reno, NV January 5–8, 2004 DEVELOPMENT OF A HIGHER-ORDER SOLVER FOR AERODYNAMIC APPLICATIONS