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  • 1
    Publication Date: 2019-07-13
    Description: 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.
    Keywords: Aeronautics (General); Fluid Mechanics and Thermodynamics
    Type: AIAA Paper-2014-0118 , NF1676L-17865 , AIAA Aerospace Sciences Meeting; Jan 13, 2014 - Jan 17, 2014; National Harbor, MD; United States
    Format: application/pdf
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