Novel winglet design for  reduction of Vortex Formation and enhancement of aircraft efficiency

Abstract In this research paper, we focus on creating a new winglet design to decrease vortex generation and consequently, reduce induced drag. This innovative winglet for aircraft wings helps improve overall efficiency. Winglets are aerodynamic components that are attached at the wingtips and play a crucial role in reducing drag and minimizing vortex formation, such as tip vortices, thus enhancing fuel economy. The main objective of this research paper is to mitigate the hindering effect on aircraft performance, namely, the reduction of detrimental vortices. The methodology of this research paper involves the use of software like CATIA for design and ANSYS software for analysis. The design process includes the creation of different design iterations of winglet designs with specific parameters, intending to reduce vortex formation and increase lift. Subsequent analyses were conducted on each design iteration to test performance, lift, and drag variations using ANSYS software. The results of analysis will be presented, highlighting the performance of each winglet design in comparison to the baseline wing. The study aims to identify the most efficient winglet design, aiming to minimize vortex and drag generation while maximizing lift and other aerodynamic parameters to increase overall efficiency. The study's implications will be explored for aircraft manufacturers and operators, including the potential benefits of fuel savings and a positive environmental footprint. This research significantly contributes to the aircraft domain by offering insights into innovative winglet design formulations capable of enhancing aircraft performance. This investigation serves as a foundation for further research in the realm of winglet design to enhance the sustainability and efficiency of future aircraft.