Quero-Martin, David (2014) DLM unsteady correction using non linear CFD gust aerodynamics. DLRK 2014 - Deutscher Luft- und Raumfahrtkongress, 16.-18. Sep. 2014, Augsburg, Deutschland.
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Abstract
This paper presents an implementation of the non linear gust aerodynamics computed via CFD into the linear unsteady DLM formulation by correcting the influence coefficient matrix. This method allows using state of the art non linear computations into the well-established DLM form. Comparison between the proposed method and the original CFD computations are given. Excellent agreement is shown.
Item URL in elib: | https://elib.dlr.de/92462/ | ||||||
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Document Type: | Conference or Workshop Item (Speech) | ||||||
Title: | DLM unsteady correction using non linear CFD gust aerodynamics | ||||||
Authors: |
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Date: | 2014 | ||||||
Refereed publication: | Yes | ||||||
Open Access: | No | ||||||
Gold Open Access: | No | ||||||
In SCOPUS: | No | ||||||
In ISI Web of Science: | No | ||||||
Status: | Published | ||||||
Keywords: | gust, unsteady, transonic, AIC, correction | ||||||
Event Title: | DLRK 2014 - Deutscher Luft- und Raumfahrtkongress | ||||||
Event Location: | Augsburg, Deutschland | ||||||
Event Type: | national Conference | ||||||
Event Dates: | 16.-18. Sep. 2014 | ||||||
Organizer: | DGLR | ||||||
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 (old) | ||||||
Location: | Göttingen | ||||||
Institutes and Institutions: | Institute of Aeroelasticity > Loads Analysis and Aeroelastic Design | ||||||
Deposited By: | Quero-Martin, David | ||||||
Deposited On: | 17 Dec 2014 09:27 | ||||||
Last Modified: | 17 Dec 2014 09:27 |
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