Please use this identifier to cite or link to this item: http://hdl.handle.net/2440/126175
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dc.contributor.authorTang, D.en
dc.contributor.authorChen, L.en
dc.contributor.authorTian, Z.en
dc.contributor.authorHu, E.en
dc.date.issued2020en
dc.identifier.citationJournal of Sound and Vibration, 2020; 468:115061-1-115061-16en
dc.identifier.issn0022-460Xen
dc.identifier.issn1095-8568en
dc.identifier.urihttp://hdl.handle.net/2440/126175-
dc.descriptionAvailable online 9 November 2019en
dc.description.abstractIn this research a two-degrees-of-freedom(2-DOF) virtual stiffness-damping system (VSDS) is developed to facilitate industrial and laboratory testing of airfoil aeroelasticity instability. Other existing test-beds in this field rely on elastic elements or structures to set airfoil elasticity in tests, which can be costly and inconvenient in cases of frequent stiffness adjustment across a wide range. A possible alternative is the VSDS that utilizes electric drives to simulate structural elasticity and damping, as seen in marine and bio-mechanical engineering, which however, cannot be directly applied to airfoil aeroelasticity testing (AAT) due to operation requirements and conditions being different. Therefore, in this study a new VSDS is developed specifically for AAT. Firstly, the concept of 1-DOF VSDS is extended to 2 DOFs, with the dynamics coupling between each DOF addressed at the stage of operation principle determination, by the proposed direct force/torque regulation with force/torque feedback. Secondly, resolution loss in position/velocity measurement is identified as a main problem associated with the non-reduction transmission required, and is solved by a modified extended-state observer (MESO) proposed for fast position/velocity estimation. Thirdly, systemidentification and calibration procedures involved in developing the new VSDS are reduced to minimum through a robust force/torque tracking controller design, with detailed numerical study on parametric analysis given. As validated in wind-tunnel experiments the new VSDS can closely track the desired force/torque and provide satisfactory virtual stiffness and damping in AAT.en
dc.description.statementofresponsibilityDifan Tang, Lei Chen, Zhao Feng Tian, Eric Huen
dc.language.isoenen
dc.publisherElsevieren
dc.rights© 2019 Elsevier Ltd. All rights reserved.en
dc.subjectAeroelasticity; Virtual damping; Virtual stiffnessen
dc.titleDeveloping a virtual stiffness-damping system for airfoil aeroelasticity testingen
dc.typeJournal articleen
dc.identifier.rmid1000007893en
dc.identifier.doi10.1016/j.jsv.2019.115061en
dc.identifier.pubid506826-
pubs.library.collectionMechanical Engineering publicationsen
pubs.library.teamDS03en
pubs.verification-statusVerifieden
pubs.publication-statusPublisheden
dc.identifier.orcidTang, D. [0000-0002-7143-0441]en
dc.identifier.orcidChen, L. [0000-0002-2269-2912]en
dc.identifier.orcidTian, Z. [0000-0001-9847-6004]en
dc.identifier.orcidHu, E. [0000-0002-7390-0961]en
Appears in Collections:Mechanical Engineering publications

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