Unstructured-Mesh Discretizations and Solvers for Computational Aerodynamics
Author:
Affiliation:
1. University of Wyoming, Laramie, Wyoming 82071-3295
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.34681
Reference96 articles.
1. On the numerical solution of nonlinear problems in fluid dynamics by least squares and finite element methods (II). Application to transonic flow simulations
2. Finite volume solution of the two-dimensional Euler equations on a regular triangular mesh
3. Calculation of Inviscid Transonic Flow over a Complete Aircraft
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