Aerodynamic Performance Enhancement of a Low-Aspect-Ratio Flying-Wing UCAV through 30° Blended Winglet Integration

Aerodynamic Performance Enhancement of a Low-Aspect-Ratio Flying-Wing UCAV through 30° Blended Winglet Integration. 1.Designed a UCAV concept with and without winglet using SolidWorks1. 2.Analysis aerodynamics performance with and without winglet using Ansys Fluent 3.Mesh independent study and running over 30 simulations 4.Prepared detailed technical reports for this project and suggested to be a research paper