Supersonic inlet calculations using an upwind finite-volume method on adaptive unstructured grids
Author:
Affiliation:
1. Texas, University, Arlington
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1989-113
Reference10 articles.
1. [l] Kennon, S.R. "Numerical Solution of Weak Forms of Conservation Laws on Optimal Unstructured Triangular Grids," Ph.D. Thesis,Department of Aerospace Engineering and Engineering Mechanics, Universityof Texas at Austin, Austin, Texas,August, 1987.
2. Calculation of Inviscid Transonic Flow over a Complete Aircraft
3. A vectorized Delaunay triangulation scheme for non-convex domains with automatic nodal point generation
4. Approximate Riemann solvers, parameter vectors, and difference schemes
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