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 …

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 …

Assessment of hydrogen transport aircraft: Effects of fuel tank integration

G Onorato, P Proesmans, MFM Hoogreef - CEAS Aeronautical Journal, 2022 - Springer
Zero-carbon-dioxide-emitting hydrogen-powered aircraft have, in recent decades, come
back on the stage as promising protagonists in the fight against global warming. The main …

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 …

Rans-based aerodynamic shape optimization of a wing considering propeller–wing interaction

SS Chauhan, JRRA Martins - Journal of Aircraft, 2021 - arc.aiaa.org
The recent growth of interest in hybrid-electric and fully electric aircraft has led to a renewed
focus on the design and optimization of propeller aircraft. Considering propeller–wing …

Adaptive initial sizing method and safety assessment for hybrid-electric regional aircraft

N Moebs, D Eisenhut, E Windels, J Van der Pols… - Aerospace, 2022 - mdpi.com
In the wake of many climate-friendly initiatives, the aviation sector must become more
sustainable. A potential path for regional airliners could be the installation of hybrid-electric …

RANS-Based Aerodynamic Shape Optimization of a Wing with a Propeller in Front of the Wingtip

SS Chauhan, JRRA Martins - Aerospace, 2024 - mdpi.com
Accounting for propeller–wing interaction allows for the design of more efficient propeller
aircraft through strategic propulsion integration. In this paper, the cruise drag of a wing with a …

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 …

Aero-propulsive efficiency requirements for turboelectric transport aircraft

R de Vries, M Hoogreef, R Vos - AIAA Scitech 2020 Forum, 2020 - arc.aiaa.org
In this paper a design-of-experiments is performed with the objective of determining the
improvements in aeropropulsive efficiency required for a reduction in the energy …

[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 …