A numerical simulation of transonic flows over complete ASKA aircraft configuration is performed. A computational grid system is constructed using the algebraic multi-block method. The Euler equations are numerically solved by the upwind finite volume scheme.
Aerodynamic Simulation for Complete ASKA Aircraft Configuration
1987
4 pages
Report
Keine Angabe
Englisch
Numerical Simulation of Compressible Flow Field about Complete ASKA Aircraft Configuration
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