Adaptive inviscid flow solutions for aerospace geometries on efficiently generated unstructured tetrahedral meshes
Author:
Affiliation:
1. Univ. College, Swansea, United Kingdom
2. NSF Engineering Research Center, Mississippi State, MS
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1993-3390
Reference15 articles.
1. Finite element Euler computations in three dimensions
2. The computation of three-dimensional flows using unstructured grids
3. N. P. Weatherill, 0.Hassan andD.L. Marcum,'Calculation of steady compressible flowfields with the finite element method',AIAAPaper -93-0341.
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