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Aeroelastic Modeling and Control of an Experimental Flexible Wing

Pusch, Manuel and Ossmann, Daniel and Kier, Thiemo and Dillinger, Johannes and Tang, Martin and Lübker, Jannis (2019) Aeroelastic Modeling and Control of an Experimental Flexible Wing. AIAA SciTech Forum, 7.1.2019-11.1.2019, San Diego, USA. DOI: 10.2514/6.2019-0131

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Item URL in elib:https://elib.dlr.de/127643/
Document Type:Conference or Workshop Item (Speech)
Title:Aeroelastic Modeling and Control of an Experimental Flexible Wing
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Pusch, ManuelManuel.Pusch (at) DLR.deUNSPECIFIED
Ossmann, Danieldaniel.ossmann (at) dlr.deUNSPECIFIED
Kier, ThiemoThiemo.Kier (at) DLR.deUNSPECIFIED
Dillinger, Johannesjohannes.dillinger (at) dlr.deUNSPECIFIED
Tang, MartinMartin.Tang (at) dlr.deUNSPECIFIED
Lübker, Jannisjannis.luebker (at) dlr.deUNSPECIFIED
Date:January 2019
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
DOI :10.2514/6.2019-0131
Status:Published
Keywords:gust load alleviation, windtunnel experiment
Event Title:AIAA SciTech Forum
Event Location:San Diego, USA
Event Type:international Conference
Event Dates:7.1.2019-11.1.2019
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Systems and Cabin
Location: Oberpfaffenhofen
Institutes and Institutions:Institute of System Dynamics and Control > Aircraft System Dynamics
Institute of Aeroelasticity > Aeroelastic Experiments
Institute of Aeroelasticity > Loads Analysis and Aeroelastic Design
Institute of Aeroelasticity > Structural Dynamics and System Identification
Deposited By: Pusch, Manuel
Deposited On:04 Jun 2019 10:46
Last Modified:31 Jul 2019 20:25

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