Aerodynamic Performance Analysis of a Dual-Purpose Aircraft for Targeted Payload Delivery

Abstract

The landscape of modern delivery services is changing due to the convergence of technological innovation and changing customer behavior. In response to the increasing e-commerce demands and the issues created by urban congestion and environmental concerns, this study provides a conceptual design and simulation for an autonomous aerial vehicle customized to the complexities of modern logistics. This research examines the possibility of airborne delivery technologies to change last-mile delivery. With established delivery businesses and merchants delving into airborne distribution, the potential of using planes to avoid traffic congestion and cut carbon emissions is becoming more apparent. The center of this project is developing a customizable airborne vehicle capable of direct point-to-point delivery, reducing delays and human interaction. The paper must overcome several limitations, such as a maximum Thrust-to-Weight ratio of 0.75, a compact wingspan of less than 120 cm, and the capacity to function from semi-prepared surfaces. The aerodynamic performance of the NACA 0009 airfoil was analyzed using xlfr5 software. The maximum drag and lift coefficient was found at 10° and 8° respectively. The neutral point is located above the center of gravity of the aircraft which ensures the stability of the aircraft.