Electroactive Morphing Effects in the Aerodynamic Performance of a Cambered A320 Wing by Means of Numerical Simulation, TRPIV and Controller Design

Autor: CARVALHO, Mateus, Raibaudo, Cédric, Döll, Carsten, Mouyon, Philippe, Marouf, Abderahmane, Nadal, Clément, Harribey, Dominique, Rouchon, Jean-François, Braza, Marianna

Publikováno v: 8th European Congress on Computational Methods in Applied Science and Engineering (ECCOMAS 2020) 14th World Congress on Computational Mechanics (WCCM XIV)
8th European Congress on Computational Methods in Applied Science and Engineering (ECCOMAS 2020) 14th World Congress on Computational Mechanics (WCCM XIV), Jan 2021, En ligne, France. 2021

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::47ff20b2c5d5b6e3a8d51255a6056ae5
https://hal.science/hal-03321654

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

Reduction of vertical tail using differential thrust : Influence on flight control and certification

Autor: Nguyen, Eric, Troillard, Pierre, Jézégou, Joël, Alazard, Daniel, Pastor, Philippe, Döll, Carsten

Publikováno v: AEGATS 2018
AEGATS 2018, Oct 2018, TOULOUSE, France

International audience; The flight control characteristics and certification compliance of a Distributed Electric Propulsion (DEP) aircraft using differential thrust is studied through exploration of flight envelops. Identification of critical flight

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=od_______212::dfb4992d50529c3eef21d0f0ca6745f5
https://hal.archives-ouvertes.fr/hal-02183315

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An Algorithm for Computing an Upper Bound of the Peak Values of μ

Autor: Magni, Jean-François, Biannic, Jean-Marc, Döll, Carsten

Publikováno v: In IFAC Proceedings Volumes August 2001 34(13):345-349