Possibility-Based Sizing Method for Hybrid Electric Aircraft
At the early stage of aircraft design, the sizing process plays a critical role in determining key parameters such as mass, geometry, and propulsion system characteristics based on design requirements. However, existing sizing methods, relying on historical data, assumptions, and low-fidelity models...
Saved in:
| Main Authors: | Zin Win Thu, Maxim Tyan, Yong-Hyeon Choi, Mohammad Irfan Alam, Jae-Woo Lee |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
IEEE
2025-01-01
|
| Series: | IEEE Access |
| Subjects: | |
| Online Access: | https://ieeexplore.ieee.org/document/10845774/ |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Aircraft Design Capabilities for a System-of-Systems Approach (eVTOL and Seaplane Design)
by: Michele Tuccillo, et al.
Published: (2025-03-01) -
Acausal Fuel Cell Simulation Model for System Integration Analysis in Early Design Phases
by: Leonardo Cavini, et al.
Published: (2024-10-01) -
Preliminary Design of Regional Aircraft—Integration of a Fuel Cell-Electric Energy Network in SUAVE
by: Jakob Schlittenhardt, et al.
Published: (2025-03-01) -
Retrofitted Hydrogen-Electric Propulsion Aircraft: Performance Simulation of Critical Operating Conditions
by: Wim Lammen, et al.
Published: (2025-01-01) -
Development of Hydrogen-Based Aviation Power in China
by: Jun Cao, et al.
Published: (2025-04-01)