Predesign Considerations for the DC Link Voltage Level of the CENTRELINE Fuselage Fan Drive Unit
Electric propulsion (EP) systems offer considerably more degrees of freedom (DOFs) within the design process of aircraft compared to conventional aircraft engines. This requires large, computationally expensive design space explorations (DSE) with coupled models of the single components to incorpora...
Main Authors: | Stefan Biser, Guido Wortmann, Swen Ruppert, Mykhaylo Filipenko, Mathias Noe, Martin Boll |
---|---|
Format: | Article |
Language: | English |
Published: |
MDPI AG
2019-11-01
|
Series: | Aerospace |
Subjects: | |
Online Access: | https://www.mdpi.com/2226-4310/6/12/126 |
Similar Items
-
Learning colon centreline from optical colonoscopy, a new way to generate a map of the internal colon surface
by: Mohammad Ali Armin, et al.
Published: (2019-10-01) -
Comparative Analysis and Optimization of Technical and Weight Parameters of Turbo-Electric Propulsion Systems
by: Mykhaylo Filipenko, et al.
Published: (2020-07-01) -
How does road marking in horizontal curves influence driving behaviour?
by: Pavel Havránek, et al.
Published: (2020-05-01) -
A Conceptual Design and Optimization Approach for Distributed Electric Propulsion eVTOL Aircraft Based on Ducted-Fan Wing Unit
by: Tielin Ma, et al.
Published: (2022-11-01) -
Simulation Analysis of DC Fault Interruption Characteristics of Superconducting Electric Aircraft Propulsion
by: Muhammad Junaid, et al.
Published: (2024-01-01)