Conceptual design and comparison of hybrid electric propulsion systems for small aircraft
- Standort
-
Deutsche Nationalbibliothek Frankfurt am Main
- ISSN
-
1869-5590
- Umfang
-
Online-Ressource
- Sprache
-
Englisch
- Anmerkungen
-
online resource.
- Erschienen in
-
Conceptual design and comparison of hybrid electric propulsion systems for small aircraft ; volume:12 ; number:4 ; day:16 ; month:8 ; year:2021 ; pages:907-922 ; date:11.2021
CEAS Aeronautical Journal / Confederation of European Aerospace Societies ; 12, Heft 4 (16.8.2021), 907-922, 11.2021
- Urheber
- Beteiligte Personen und Organisationen
-
SpringerLink (Online service)
- DOI
-
10.1007/s13272-021-00536-4
- URN
-
urn:nbn:de:101:1-2022011505405877422067
- Rechteinformation
-
Open Access; Der Zugriff auf das Objekt ist unbeschränkt möglich.
- Letzte Aktualisierung
-
15.08.2025, 07:27 MESZ
Datenpartner
Dieses Objekt wird bereitgestellt von:
Deutsche Nationalbibliothek. Bei Fragen zum Objekt wenden Sie sich bitte an den Datenpartner.
Deutsche Nationalbibliothek. Bei Fragen zum Objekt wenden Sie sich bitte an den Datenpartner.
Beteiligte
- Köhler, Jo
- Jeschke, Peter
- SpringerLink (Online service)
Ähnliche Objekte (12)
Hummingbird Hybrid - Micro Hybrid Electric Aircraft Propulsion System
Evaluating Aircraft with Electric and Hybrid Propulsion
Conceptual design and comparison of hybrid electric propulsion systems for small aircraft
Hybrid-electric propulsion systems for small unmanned aircraft
Hybrid-electric propulsion systems for small unmanned aircraft
Ducted fans for hybrid electric propulsion of small aircraft
Ducted fans for hybrid electric propulsion of small aircraft
Conceptual design of operation strategies for hybrid electric aircraft
Sizing of the series hybrid-electric propulsion system of general aviation aircraft
Basic Comparison of Three Aircraft Concepts: Classic Jet Propulsion, Turbo-Electric Propulsion and Turbo-Hydraulic Propulsion
Evaluation of electric propulsion systems in preliminary aircraft design
Electric Propulsion for Regional Aircraft - Critical Components and Challenges
Hummingbird Hybrid - Micro Hybrid Electric Aircraft Propulsion System
Evaluating Aircraft with Electric and Hybrid Propulsion
Conceptual design and comparison of hybrid electric propulsion systems for small aircraft
Hybrid-electric propulsion systems for small unmanned aircraft
Hybrid-electric propulsion systems for small unmanned aircraft
Ducted fans for hybrid electric propulsion of small aircraft
Ducted fans for hybrid electric propulsion of small aircraft
Conceptual design of operation strategies for hybrid electric aircraft
Sizing of the series hybrid-electric propulsion system of general aviation aircraft
Basic Comparison of Three Aircraft Concepts: Classic Jet Propulsion, Turbo-Electric Propulsion and Turbo-Hydraulic Propulsion
Evaluation of electric propulsion systems in preliminary aircraft design
Electric Propulsion for Regional Aircraft - Critical Components and Challenges
Hummingbird Hybrid - Micro Hybrid Electric Aircraft Propulsion System
Evaluating Aircraft with Electric and Hybrid Propulsion
Conceptual design and comparison of hybrid electric propulsion systems for small aircraft
Hybrid-electric propulsion systems for small unmanned aircraft
Hybrid-electric propulsion systems for small unmanned aircraft
Ducted fans for hybrid electric propulsion of small aircraft
Ducted fans for hybrid electric propulsion of small aircraft
Conceptual design of operation strategies for hybrid electric aircraft
Sizing of the series hybrid-electric propulsion system of general aviation aircraft
Basic Comparison of Three Aircraft Concepts: Classic Jet Propulsion, Turbo-Electric Propulsion and Turbo-Hydraulic Propulsion
Evaluation of electric propulsion systems in preliminary aircraft design