Zobrazeno 1 - 10 of 17 pro vyhledávání: '"Schmollgruber Peter"'
1
Akademický článek
Preliminary Sizing of a Medium Range Blended Wing-Body using a Multidisciplinary Design Analysis Approach
Autor: Sgueglia Alessandro, Schmollgruber Peter, Benard Emmanuel, Bartoli Nathalie, Morlier Joseph
Publikováno v: MATEC Web of Conferences, Vol 233, p 00014 (2018)
The aviation's goal for the next decades is to drastically reduce emissions, but to achieve this goal a breakdown in aircraft design has to be considered. One of the most promising concepts is the Blended Wing- Body, which integrates aerodynamics, pr
Externí odkaz: https://doaj.org/article/8ff9568c1f9149fba744246707d763ba
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4
An Overview of the Conceptual Design Studies of Hybrid Electric Propulsion Air Vehicles in the Frame of Clean Sky 2 Large Passenger Aircraft
Autor: Zill, Thomas, Iwanizki, Michael, Schmollgruber, Peter, Defoort, Sebastien, Döll, Carsten, Hoogreef, M.F.M., de Vries, R., Vankan, Jos, Lammen, Wim
Publikováno v: Aerospace Europe Conference 2020. Bordeaux, France
Aerospace Europe Conference 2020
In the Clean Sky 2 Large Passenger Aircraft (LPA) program the potential of innovative hybrid electric propulsion (HEP) air vehicle concepts has been investigated by the projects ADEC (Advanced Engine and Aircraft Configuration) and NOVAIR (Novel Airc
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::09297a1d99c880bf6f21caed17614a06
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5
Framework development for robust design of novel aircraft concept
Autor: Saporito, Marco, Da Ronch , Andrea, Schmollgruber, Peter, Bartoli, Nathalie
Publikováno v: 3AF Aerospace Europe Conference 2020
3AF Aerospace Europe Conference 2020, Feb 2020, BORDEAUX, France
International audience; One of the challenges in Multidisciplinary Design Analysis and Optimization is raised by the fidelity of the methods and tools used within each single discipline. This element, introducing uncertainty in predictions, is neglec
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::65f4efda67053588fbc2b2854f5970da
https://hal.archives-ouvertes.fr/hal-02904365
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6
A comparative study of different propulsion models for hybrid electric aircraft
Autor: Palladino, Vincenzo, Bartoli, Nathalie, Dubreuil, Sylvain, Bénard, Emmanuel, Pommier-Budinger, Valérie, Jordan, Arnaud, Schmollgruber, Peter, Defoort, Sébastien
Publikováno v: 3AF Aerospace Europe Conference 2020
3AF Aerospace Europe Conference 2020, Feb 2020, BORDEAUX, France
International audience; This paper addresses the topic of multidisciplinary analysis (MDA) applied to hybrid electric aircraft (HEA) design focusing on the analysis of multi-fidelity models for hybrid electric powertrain design. The motivation behind
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::833d0cd9c5e3f928f73b292bf11c821c
https://hal.archives-ouvertes.fr/hal-02904367
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7
Akademický článek
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8
Amélioration du processus de conception avion en prenant en compte les contraintes de certification et des simulations de mission complètes
Autor: Schmollgruber, Peter
Publikováno v: Engineering Sciences [physics]. Doctorat de l'Université de Toulouse délivré par l'Institut Supérieur de l’Aéronautique et de l’Espace (ISAE), 2018. English
La conception d'un nouvel avion est initiée durant la phase avant-projet. Dans un premier temps, les concepteurs d’aéronefs identifient un ensemble de concepts potentiels pouvant répondre aux exigences du client en s’appuyant sur des informati
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::a72b53716d08a91acb1771812ebcec84
https://hal.archives-ouvertes.fr/tel-02146110/file/DTIS19091.1558348214.pdf
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9
Enhancement of the conceptual aircraft design process through certification constraints management and full mission simulations
Autor: Schmollgruber, Peter
Publikováno v: Engineering Sciences [physics]. Doctorat de l'Université de Toulouse délivré par l'Institut Supérieur de l’Aéronautique et de l’Espace (ISAE), 2018. English
In the field of civil transport aircraft, environmental constraints set challenging goals in terms of fuel consumption for the next generations of airplanes. With the “tube and wing” configuration offering low expectations on further improvements
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::138e1830496075ceb475e00c834b9c4d
https://hal.archives-ouvertes.fr/tel-02146110
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10
Exploration and Sizing of a Large Passenger Aircraft with Distributed Electric Ducted Fans
Autor: Sgueglia , Alessandro, Schmollgruber , Peter, Bartoli , Nathalie, Atinault , Olivier, Bénard , Emmanuel, Morlier , Joseph
Publikováno v: Proceedings of AIAA Aerospace Sciences Meeting (Scitech)
AIAA-Scitech 2018
AIAA-Scitech 2018, Jan 2018, Kissimmee, United States. Proceedings of AIAA Aerospace Sciences Meeting (Scitech), pp. 1-33, 2018
International audience; In order to reduce the CO2 emissions, a disruptive concept in aircraft propulsion has to be considered. As studied in the past years hybrid distributed electric propulsion is apromising option. In this work the feasibility of
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::8774231fe286e79e626223bfa25264f5
https://oatao.univ-toulouse.fr/19580/
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