نتائج البحث - "Wortmann, Guido"

1

Patent

Electric drive system for an aircraft with a minimal yawing moment

2

Proof of concept study for fuselage boundary layer ingesting propulsion

المؤلفون: Seitz, Arne, Habermann, Anaïs, Peter, Fabian, Troeltsch, Florian, Castillo Pardo, Alejandro, Della Corte, Biagio, Van Sluis, Martjin, Goraj, Zdobyslaw, Kowalski, Mariusz, Zhao, Xin, 1986, Grönstedt, Tomas, 1970, Bijewitz, Julian, Wortmann, Guido

المصدر: Aerospace. 8(1):1-65

مصطلحات موضوعية: Turbo-electric, Collaborative research, Boundary layer ingestion, Propulsive fuselage, Proof-ofconcept, Wake-filling, Multi-disciplinary aircraft design, Fan rig, Wind tunnel

وصف الملف: electronic

URL الوصول: https://research.chalmers.se/publication/522218
https://research.chalmers.se/publication/522218/file/522218_Fulltext.pdf

View record in SwePub

3

Academic Journal

The Enabling Technologies for a Quasi-Zero Emissions Commuter Aircraft

المؤلفون: Ciliberti, Danilo, Vecchia, Pierluigi Della, Memmolo, Vittorio, Nicolosi, Fabrizio, Wortmann, Guido, Ricci, Fabrizio

المساهمون: Ciliberti, Danilo, Vecchia, Pierluigi Della, Memmolo, Vittorio, Nicolosi, Fabrizio, Wortmann, Guido, Ricci, Fabrizio

مصطلحات موضوعية: aerodynamics, propulsion, aero-propulsive interactions, energy storage, airframe

Relation: info:eu-repo/semantics/altIdentifier/wos/WOS:000817712800001; volume:9; issue:6; firstpage:319; journal:AEROSPACE; info:eu-repo/grantAgreement/EC/H2020/864551; http://hdl.handle.net/11588/887952; info:eu-repo/semantics/altIdentifier/scopus/2-s2.0-85137220451; https://www.mdpi.com/2226-4310/9/6/319

الاتاحة: http://hdl.handle.net/11588/887952
https://doi.org/10.3390/aerospace9060319
https://www.mdpi.com/2226-4310/9/6/319

View record in BASE

4

Academic Journal

Predesign Considerations for the DC Link Voltage Level of the CENTRELINE Fuselage Fan Drive Unit

المؤلفون: Biser, Stefan, Wortmann, Guido, Ruppert, Swen, Filipenko, Mykhaylo, Noe, Mathias, Boll, Martin

المصدر: Aerospace, 6 (12), Art. Nr.: 126 ; ISSN: 2226-4310

مصطلحات موضوعية: electric propulsion, aircraft, CENTRELINE, DC link voltage level, analytical model, design space exploration, ddc:530, Physics, info:eu-repo/classification/ddc/530

وصف الملف: application/pdf

Relation: info:eu-repo/semantics/altIdentifier/wos/000505768100003; info:eu-repo/semantics/altIdentifier/issn/2226-4310; https://publikationen.bibliothek.kit.edu/1000129495; https://publikationen.bibliothek.kit.edu/1000129495/101946155; https://doi.org/10.5445/IR/1000129495

الاتاحة: https://publikationen.bibliothek.kit.edu/1000129495
https://publikationen.bibliothek.kit.edu/1000129495/101946155
https://doi.org/10.5445/IR/1000129495

View record in BASE

5

Investigating the Dynamic Response of Hybrid-Electric Propulsion Systems for Flight Control Application

المؤلفون: Wortmann, Guido

المساهمون: Holzapfel, Florian, Wood apple, Florian, Hornung, Mirko

الاتاحة: http://data.europeana.eu/aggregation/europeana/2048441/item_GKNLUAK6KQASAFHHQWFZRLGTHTBOSAC6

View record in Europeana

6

Integration Aspects for Large Generators into Turbofan Engines for a Turbo-electric Propulsive Fuselage Concept

المؤلفون: Merkler, Rasmus, Samuelsson, Sebastian, 1987, Wortmann, Guido

المصدر: 24th ISABE Conference, Canberra, Australia 24th International Symposium on Air Breathing Engines (ISABE 2019). :536-552

مصطلحات موضوعية: main geared turbofan engine considerations, Large power offtake, thermal management concept, power generation unit integration concept

URL الوصول: https://research.chalmers.se/publication/512631

7

Adaption of a Turbofan Engine for High Power Offtakes for a Turbo-electric Propulsive Fuselage Concept

المؤلفون: Samuelsson, Sebastian, 1987, Petit, Olivier, 1980, Merkler, Rasmus, Wortmann, Guido

المصدر: 24th ISABE Conference, Canberra, Australia ISABE 2019 Papers.

مصطلحات موضوعية: large power offtake, aircraft engine conceptual design, free power turbine, propulsive fuselage, geared turbofan, aircraft engine performance, turbo-electric aircraft

URL الوصول: https://research.chalmers.se/publication/512630
https://drive.google.com/drive/folders/1PZaMaLOLsybB3KFLmvP8hwM_lwmk3e4B

8

Investigating the Dynamic Response of Hybrid-Electric Propulsion Systems for Flight Control Application

المؤلفون: Wortmann, Guido

المساهمون: Hornung, Mirko (Prof. Dr.), Holzapfel, Florian (Prof. Dr.)

مصطلحات موضوعية: Ingenieurwissenschaften, hybrid, aircraft propulsion, flight control, ddc:620, hybrid, Flugantriebe, Flugsteuerung

وصف الملف: application/pdf

URL الوصول: https://explore.openaire.eu/search/publication?articleId=od_______518::5b03281a7da940345638c4a8342f0732
https://mediatum.ub.tum.de/1293023

View record in OpenAIRE

9

Concept validation study for fuselage wake-filling propulsion integration

المؤلفون: Seitz, Arne, Peter, Fabian, Bijewitz, Julian, Habermann, Anaïs, Goraj, Zdobyslaw, Kowalski, Mariusz, Pardo, Alejandro Castillo, Hall, Cesare, Meller, Frank, Merkler, Rasmus, Petit, Olivier, 1980, Samuelsson, Sebastian, 1987, Corte, Biagio Della, Van Sluis, Martjin, Wortmann, Guido, Dietz, Martin

المصدر: 31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018, Belo Horizonte, Brazil 31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018.

مصطلحات موضوعية: Propulsion Integration, Propulsive Fuselage, Wake-Filling, Boundary Layer Ingestion

URL الوصول: https://research.chalmers.se/publication/508475