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Quero, David and Krüger, Wolf and Jenaro, Guillermo (2016) A Reduced Order Model for Aeroelastic Response Prediction to Continuous Turbulence Encounter including CFD Aerodynamics. AIAA Aviation, 16.-17. Juni 2016, Washington DC, USA.
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Abstract
Abstract In this paper a frequency domain Reduced Order Model (ROM) to compute the aeroelastic response of a free flexible aircraft flying through continuous turbulence while including high fidelity aerodynamics is presented. It is based on the correction of the unsteady Aerodynamic Influence Coefficient (AIC) matrices. Simulations on both rigid and flexible aircraft have been carried out and the results have been validated against full order time domain simulations for a representative transonic case.
| Item URL in elib: | https://elib.dlr.de/107259/ | ||||||||||||
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| Document Type: | Conference or Workshop Item (Speech) | ||||||||||||
| Title: | A Reduced Order Model for Aeroelastic Response Prediction to Continuous Turbulence Encounter including CFD Aerodynamics | ||||||||||||
| Authors: |
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| Date: | 2016 | ||||||||||||
| Refereed publication: | Yes | ||||||||||||
| Open Access: | No | ||||||||||||
| Gold Open Access: | No | ||||||||||||
| In SCOPUS: | No | ||||||||||||
| In ISI Web of Science: | No | ||||||||||||
| Status: | Published | ||||||||||||
| Keywords: | ROM, gust encounter, continuous turbulence | ||||||||||||
| Event Title: | AIAA Aviation | ||||||||||||
| Event Location: | Washington DC, USA | ||||||||||||
| Event Type: | international Conference | ||||||||||||
| Event Dates: | 16.-17. Juni 2016 | ||||||||||||
| Organizer: | AIAA | ||||||||||||
| 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 - Flight Physics | ||||||||||||
| Location: | Göttingen | ||||||||||||
| Institutes and Institutions: | Institute of Aeroelasticity > Loads Analysis and Aeroelastic Design | ||||||||||||
| Deposited By: | Quero-Martin, David | ||||||||||||
| Deposited On: | 28 Nov 2016 16:28 | ||||||||||||
| Last Modified: | 28 Nov 2016 16:28 |
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