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DLM unsteady correction using non linear CFD gust aerodynamics

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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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/
Document Type:Conference or Workshop Item (Speech)
Title:DLM unsteady correction using non linear CFD gust aerodynamics
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Quero-Martin, Daviddavid.queromartin (at) dlr.deUNSPECIFIED
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
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
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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