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A Finite Element Approach to Rotary-Wing Aeroelasticity

Gloth, G. and Hartmann, S. and Haupt, P. (1997) A Finite Element Approach to Rotary-Wing Aeroelasticity. In: International Forum on Aeroelasticity and Structural Dynamics Volume III, Volume III, pp. 143-150. CEAS - International Forum on Aeroelasticity and Structural Dynamics, 17.-20.06.1997, Rome, Italy.

Full text not available from this repository.


Item URL in elib:https://elib.dlr.de/39851/
Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=1997,
Title:A Finite Element Approach to Rotary-Wing Aeroelasticity
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Gloth, G.UNSPECIFIEDUNSPECIFIED
Hartmann, S.Universität GH KasselUNSPECIFIED
Haupt, P.Universität GH KasselUNSPECIFIED
Date:1997
Journal or Publication Title:International Forum on Aeroelasticity and Structural Dynamics Volume III
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:Volume III
Page Range:pp. 143-150
Status:Published
Keywords:rotary-wing aeroelasticity, flutter calculations, finite elements
Event Title:CEAS - International Forum on Aeroelasticity and Structural Dynamics, 17.-20.06.1997, Rome, Italy
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Space (old)
HGF - Program Themes:W RP - Raumtransport
DLR - Research area:Space
DLR - Program:W RP - Raumtransport
DLR - Research theme (Project):UNSPECIFIED
Location: Göttingen
Institutes and Institutions:Institute of Aeroelasticity
Deposited By: DLR-Beauftragter, elib
Deposited On:02 Apr 2006
Last Modified:27 Apr 2009 10:56

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