A review of concepts, benefits, and challenges for future electrical propulsion-based aircraft

S Sahoo, X Zhao, K Kyprianidis - Aerospace, 2020 - mdpi.com
Electrification of the propulsion system has opened the door to a new paradigm of
propulsion system configurations and novel aircraft designs, which was never envisioned …

[HTML][HTML] Aerodynamic interaction between propellers of a distributed-propulsion system in forward flight

R de Vries, N van Arnhem, T Sinnige, R Vos… - Aerospace Science and …, 2021 - Elsevier
This article describes an experimental investigation of the aerodynamic interaction that
occurs between distributed propellers in forward flight. To this end, three propellers were …

Regional pathways for all-electric aircraft to reduce aviation sector greenhouse gas emissions

J Eaton, M Naraghi, JG Boyd - Applied Energy, 2024 - Elsevier
Forecasted growth in aviation sector emissions has motivated research into reduced-
emissions aircraft designs. All-electric aircraft (AEA) are of unique interest due to negligible …

A comparison of hybrid-electric aircraft sizing methods

DF Finger, R de Vries, R Vos, C Braun, C Bil - AIAA scitech 2020 forum, 2020 - arc.aiaa.org
The number of case studies focusing on hybrid-electric aircraft is steadily increasing, since
these configurations are thought to lead to lower operating costs and environmental impact …

Generic design methodology for vertical takeoff and landing aircraft with hybrid-electric propulsion

D Lee, D Lim, K Yee - Journal of Aircraft, 2022 - arc.aiaa.org
This paper proposes a conceptual methodology for designing vertical takeoff and landing
aircraft with a hybrid-electric propulsion system as an alternative to facilitate intercity …

Cross-validation of hybrid-electric aircraft sizing methods

DF Finger, R de Vries, R Vos, C Braun, C Bil - Journal of Aircraft, 2022 - arc.aiaa.org
The number of studies on hybrid-electric aircraft is steadily increasing because these
configurations can lead to lower operating costs and environmental impact than traditional …

Engineering method to estimate the blade loading of propellers in nonuniform flow

N van Arnhem, R de Vries, T Sinnige, R Vos… - AIAA Journal, 2020 - arc.aiaa.org
Advances in aerodynamic and propulsive efficiency of future aircraft can be achieved by
strategic installation of propellers near the airframe. This paper presents a robust and …

Aerodynamic performance benefits of over-the-wing distributed propulsion for hybrid-electric transport aircraft

R de Vries, R Vos - Journal of Aircraft, 2023 - arc.aiaa.org
The goal of this study is to analyze how the aeropropulsive benefits of an over-the-wing
distributed-propulsion (OTWDP) system at the component level translate into an …

Synthesis of aero-propulsive interaction studies applied to conceptual hybrid-electric aircraft design

M Hoogreef, R de Vries, T Sinnige, R Vos - AIAA Scitech 2020 Forum, 2020 - arc.aiaa.org
This paper presents a synthesis of aero-propulsive interaction studies performed at Delft
University of Technology, applied to conceptual aircraft designs with distributed hybrid …

[PDF][PDF] Methodology for Multidisciplinary Aircraft Design under Consideration of Hybrid-Electric Propulsion Technology

DF Finger - 2020 - researchgate.net
Against a background of increasing energy demand and rising fuel prices, hybrid-electric
propulsion systems have the potential to significantly reduce emissions of aircraft …