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Aerodynamic Analysis of Box Wing Configuration for Unmanned Aircraft System (UAS)

Computational Fluid Dynamic (CFD) analysis is performed to determine the ideal box wing configuration for small UAS.

Project Details

Campus: Worldwide Campus
College: Worldwide College of Aviation
Department: WENSC, Worldwide College of Aviation, Worldwide Campus
Type: Faculty-Staff
Start Date: 01/01/2012
End Date: 08/31/2014
​Computational Fluid Dynamic (CFD) analysis is performed to determine the ideal box wing configuration for small UAS.