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