Project Abstract: 

Urban Air Mobility (UAM) emerges as a promising solution to combat urban traffic congestion, offering a safe and efficient alternative to traditional ground transportation, especially in emergency high-speed air transport scenarios. The sizing and design of such aircraft remain the need of time to establish the method. This paper presents the conceptual design and analysis of a four-seater autonomous electric Vertical Take-Off and Landing (eVTOL) aircraft, envisioned for up to 250 km range. The study explores the design feasibility under specific mission requirements and varying environmental conditions. It uses the Vortex Lattice Method for aerodynamic analysis, focusing on critical aircraft components such as wings and propellers and evaluating their overall performance. This project aims to contribute to the evolving field of UAM by providing insights into the feasibility, efficiency, and environmental implications of eVTOL aircraft in urban settings.