Structural batteries in aviation: A preliminary sizing methodology

CED Riboldi, L Trainelli, F Biondani - Journal of Aerospace …, 2020 - ascelibrary.org
A significant research effort in aviation is currently focused on the integration of electric or
hybrid-electric power-trains onboard aircraft in an effort to improve efficiency and …

[PDF][PDF] A general preliminary sizing procedure for pure-electric and hybrid-electric airplanes

L Trainelli, CED Riboldi, F Salucci… - 1st Aerospace Europe …, 2020 - re.public.polimi.it
Galileo 2009 Page 1 1 A GENERAL PRELIMINARY SIZING PROCEDURE FOR PURE-ELECTRIC
AND HYBRID-ELECTRIC AIRPLANES Lorenzo Trainelli, Carlo ED Riboldi, Francesco Salucci …

Fuel cell hybrid-electric aircraft: design, operational, and environmental impact

AE Scholz, J Michelmann, M Hornung - Journal of Aircraft, 2023 - arc.aiaa.org
To reduce the environmental footprint of the aviation industry, aircraft with new propulsion
systems are increasingly under consideration. In this paper, the potential of a fuel cell hybrid …

From a battery-based to a PEM fuel cell-based propulsion architecture on a lightweight full electric aircraft: A Comparative Numerical Study

G Marinaro, G Di Lorenzo, A Pagano - Aerospace, 2022 - mdpi.com
The aviation sector is firmly committed to reducing harmful emissions and electric propulsion
promises to tackle both pollution and noise at the same time. More Electric Aircrafts are …

[PDF][PDF] Preliminary sizing and energy management of serial hybrid-electric airplanes

L Trainelli, F Salucci, N Rossi, CED Riboldi… - AIDAA Congress …, 2019 - academia.edu
ABSTRACT A novel methodology for the preliminary sizing of pure-electric and serial hybrid-
electric airplanes is presented, which is general and capable of dealing with propeller …

[PDF][PDF] Methodologies for the Preliminary Sizing of Hydrogen-Powered Aircraft and Supporting Airport Infrastructures

L Trainelli, CED Riboldi, G Sirtori - ICAS PROCEEDINGS, 2024 - re.public.polimi.it
This paper illustrates two general methodologies aimed at coping with the need to
preliminarily assess the feasibility, cost and performance of a future commercial aviation …

Performance and Weight Parameters Calculation for Hydrogen-and Battery-Powered Aircraft Concepts

M Janovec, V Babčan, B Kandera, K Šajbanová… - Aerospace, 2023 - mdpi.com
This article describes the creation of a program that would be useful for calculating
mathematical models in order to estimate the weight of aircraft components. Using several …

Design and aeroelastic analysis of truss-based modular wing structures

HL Silva, TA Guimarães, SG Castro - AIAA SCITECH 2023 Forum, 2023 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2023-1677. vid Modular structures come
with the promise of efficient manufacturing and reduced maintenance costs. The amount of …

[PDF][PDF] Preliminary Propulsion System Sizing Methods for PEM Fuel Cell Aircraft

D Juschus - 2021 - researchgate.net
Fuel cell (FC) aircraft are one of the most promising technological solutions for the first
generation of sustainable aircraft, especially for short and medium ranges. A FC uses …

Climate-Optimal Aircraft Design and Fleet Allocation

P Proesmans - 2024 - repository.tudelft.nl
Research into aviation-induced global warming has highlighted the significant impact of non-
CO2 effects, such as NOx emissions, water vapor emissions, and contrail formation. Unlike …