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Transonic flutter calculations for a low wing transport aircraft using the Transonic Doublet Lattice Method

Brendes, G. and Voß, R. (2001) Transonic flutter calculations for a low wing transport aircraft using the Transonic Doublet Lattice Method. IFASD, Madrid/Spain, June 5-7 2001.

Full text not available from this repository.

Abstract

This paper deals with the usage of the TDLM in the Fairchild Dornier 728JET program, the first complete aircraft application of the TDLM. At first a description of the theory of the TDLM is given. Second the procedure applied to use TDLM results during MSC/NASTRAN flutter calculations is presented. The presentation closes with a comparison of DLM and TDLM based flutter calculations.

Item URL in elib:https://elib.dlr.de/14260/
Document Type:Conference or Workshop Item (Speech)
Additional Information: LIDO-Berichtsjahr=2001,
Title:Transonic flutter calculations for a low wing transport aircraft using the Transonic Doublet Lattice Method
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Brendes, G.UNSPECIFIEDUNSPECIFIED
Voß, R.UNSPECIFIEDUNSPECIFIED
Date:2001
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Flutter, Aeroelasticity, TDLM, Unsteady Transonic Aerodynamics
Event Title:IFASD, Madrid/Spain, June 5-7 2001
Organizer:CEAS / AIAA / ICASE / NASA Langley
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:Aeronautics
DLR - Program:L ST - Starrflüglertechnologien
DLR - Research theme (Project):UNSPECIFIED
Location: Göttingen
Institutes and Institutions:Institute of Aeroelasticity
Deposited By: Erdmann, Daniela
Deposited On:16 Sep 2005
Last Modified:14 Jan 2010 21:37

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