Adaptive Mesh Euler Equation Computations of Vortex Breakdown in Delta Wing Flow
A solution method for the three-dimensional Euler equations is formulated and implemented. The solver uses an unstructured mesh of tetrahedral cells and performs adaptive refinement by mesh-point embedding to increase mesh resolution in regions of interesting flow features. The fourth-difference...
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| Format: | Technical Report |
| Language: | en_US |
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Aerospace Computational Design Lab, Dept. of Aeronautics & Astronautics, Massachusetts Institute of Technology
2012
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| Online Access: | http://hdl.handle.net/1721.1/70577 |