The paper introduces an automation process of generating a tetrahedral mesh for computational fluid dynamics (CFD) analysis of aircraft configurations in early conceptual design. The method was developed for CFD-based sonic boom analysis of supersonic configurations, but can be applied to aerodynamic analysis of aircraft configurations in any flight regime.
Automated Tetrahedral Mesh Generation for CFD Analysis of Aircraft in Conceptual Design
2014
8 pages
Report
Keine Angabe
Englisch
British Library Conference Proceedings | 2014
|Node Creation for Isotropic Tetrahedral Mesh Generation
AIAA | 2017
|