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• Organization: National Institute of Standards and Technology
• Updated: 2015-09-18 00:00:00 | Harvested: June 27, 2025 at 06:57 PM

Software for the solution of elliptic partial differential equations using finite elements with adaptive mesh refinement and multigrid techniques.

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• Organization: National Aeronautics and Space Administration
• Updated: 2025-03-31 | Harvested: June 28, 2025 at 11:42 AM

Structured multiblock grid of HIRENASD wing with medium grid density, about 10 mill grid points, 9.5 mill cells. Starting from coarse AIAA AEPW structured grid, heavily modified for: - Improved...

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