NASA NTRS · 19900020295
Unstructured mesh methods for CFD
Abstract
Mesh generation methods for Computational Fluid Dynamics (CFD) are outlined. Geometric modeling is discussed. An advancing front method is described. Flow past a two engine Falcon aeroplane is studied. An algorithm and associated data structure called the alternating digital tree, which efficiently solves the geometric searching problem is described. The computation of an initial approximation to the steady state solution of a given poblem is described. Mesh generation for transient flows is described.
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Peraire, J., Morgan, K., Peiro, J.. 1990-01-01. Unstructured mesh methods for CFD. https://ntrs.nasa.gov/citations/19900020295
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