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Experimental modal analysis of a rotating tendon-loaded helicopter blade demonstrator

Wu, Jun and Vaclav, Ondra and Lübker, Jannis and Kalow, Steffen and Riemenschneider, Johannes and Titurus, Brano (2022) Experimental modal analysis of a rotating tendon-loaded helicopter blade demonstrator. Mechanical Systems and Signal Processing, 178. Elsevier. doi: 10.1016/j.ymssp.2022.109286. ISSN 0888-3270.

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Item URL in elib:https://elib.dlr.de/186481/
Document Type:Article
Title:Experimental modal analysis of a rotating tendon-loaded helicopter blade demonstrator
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Wu, JunDepartment of Aerospace Engineering, University of Bristol, UKUNSPECIFIED
Vaclav, OndraRolls-RoyceUNSPECIFIED
Lübker, JannisJannis.Luebker (at) dlr.deUNSPECIFIED
Kalow, Steffensteffen.kalow (at) dlr.dehttps://orcid.org/0000-0002-5308-1209
Riemenschneider, JohannesJohannes.Riemenschneider (at) dlr.dehttps://orcid.org/0000-0001-5485-8326
Titurus, BranoDepartment of Aerospace Engineering, University of Bristol, UKUNSPECIFIED
Date:2022
Journal or Publication Title:Mechanical Systems and Signal Processing
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:178
DOI:10.1016/j.ymssp.2022.109286
Publisher:Elsevier
Series Name:Elsevier
ISSN:0888-3270
Status:Published
Keywords:Rotating beam-tendon Modal analysis Whirl tower Centrifugal stiffening Compressive softening
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Components and Systems
DLR - Research area:Aeronautics
DLR - Program:L CS - Components and Systems
DLR - Research theme (Project):L - Structural Materials and Design
Location: Braunschweig
Institutes and Institutions:Institute of Composite Structures and Adaptive Systems > Adaptronics
Deposited By: Stanitzek, Silke
Deposited On:23 May 2022 10:07
Last Modified:13 Jun 2022 08:02

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