Recently, a fuel cell-battery hybrid system (FBHS) has attracted considerable attention as a
potential propulsion system for electric vertical take-off and landing (eVTOL) aircraft. For the …

Recently, electric vertical takeoff and landing (eVTOL) aircraft have garnered significant
interest as a primary mode of transportation in advanced air mobility (AAM). For the …

Recent development in Electric Vertical Take-off and Landing (eVTOL) aircraft makes it a
popular design approach for urban air mobility (UAM). When designing these configurations …

This paper proposes a new multidisciplinary design optimization framework for tilt-bodies to
obtain the optimal combination of geometry and powertrain, achieving both long endurance …

This paper proposes a distributed turbo-electric hybrid propulsion system (TEHPS)
architecture for high-power and large-load air–ground aircraft (AGA). The composition of the …

View Video Presentation: https://doi. org/10.2514/6.2022-3514. vid This study develops a
fuel cell/battery hybrid system sizing methodology for eVTOL aircraft. The sizing …

View Video Presentation: https://doi. org/10.2514/6.2023-4265. vid This paper presents an
uncertainty-based sizing framework for advanced air mobility and uncertainty quantification …

Electric aircraft emerge as a promising solution to mitigate the environmental impact of the
aviation sector. The integration of electric propulsion components in such aircraft differs …

This study develops an air-cooled battery sizing method for eVTOL aircraft. The sizing
method is based on three key models for battery analysis. The first and second are voltage …

This paper proposes novel enhancements to the electric propulsion system analysis method
for electric vertical takeoff and landing (eVTOL) aircraft conceptual design by considering the …