Document Type
Paper
Abstract
The goal of this report is to analyze and test a patented wingtip vortex reduction method from the 1930’s. This report will review and explain the methods of wingtip vortex analysis, as well as the physics behind the reduction of vortices. Additionally, this paper will highlight the method used to test the design, computational fluid dynamics. Finally, by exploring the drag and vorticity difference between the two wings, this paper will explore whether or not the patented design is feasible for real-world use.
Analyzing the Impact of Venturi-Induced Wingtip Suction on the Induced Drag and Wingtip Vortex
The goal of this report is to analyze and test a patented wingtip vortex reduction method from the 1930’s. This report will review and explain the methods of wingtip vortex analysis, as well as the physics behind the reduction of vortices. Additionally, this paper will highlight the method used to test the design, computational fluid dynamics. Finally, by exploring the drag and vorticity difference between the two wings, this paper will explore whether or not the patented design is feasible for real-world use.
