Three-dimensional unsteady Euler equations solution using flux vector splitting
Author:
Affiliation:
1. Mississippi State University, Mississippi State, MS
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1984-1552
Reference15 articles.
1. Three-dimensional Euler equation simulation of propeller-wing interaction in transonic flow
2. Finite-Volume Solutions to the Euler Equations in Transonic Flow
3. 'Swafford, T. W. "Three-Dimensional, Time-Dependent, Compressible, Turbulent, Integral Boundary-Layer Equations in General Curvilinear Coordinates and Their Numerical Solution," Ph.D. Dissertation,Mississippi State University, August 1983.
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