Further applications of a three-dimensional Euler code which is able to treat arbitrary aerodynamic configurations in a wide range of flight conditions are presented. Previous publications have demonstrated the ability of the code to handle complex aircraft configurations. The present applications verify the code in flight regimes not covered by potential codes (e.g., high supersonic flow and vortex flow) by comparison with reliable, internationally reported wind tunnel experiments and analytical solutions (where available). A short description of the code is also included.
Euler Solver for Arbitrary Configurations: Further Applications
1990
12 pages
Report
Keine Angabe
Englisch
Fluid Mechanics , Aerodynamic configurations , Computational fluid dynamics , Euler equations of motion , Computer programs , Supersonic flow , Three dimensional models , Wind tunnel tests , Angle of attack , Cdc computers , Delta wings , Mathematical models , Nose cones , Transonic speed , Vortices , Foreign technology
Cartesian Euler method for arbitrary aircraft configurations
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