Publication:
Modal Parameters of Light Aircraft Wing
Modal Parameters of Light Aircraft Wing
dc.contributor.author | Vulovic, Zoran | en_US |
dc.date.accessioned | 2021-11-25T12:31:13Z | |
dc.date.available | 2021-11-25T12:31:13Z | |
dc.date.issued | 2005 | en_US |
dc.description.abstract | The main aim of this work is to extract modal parameters of a light aircraft wing. Modal parameters like modal frequency, modal damping and mode shapes characterise the dynamic response of a particular structure and can be used for determining an excess wing flexure as well as the long-term effect of fatigue. For the experimental part the response of the Piper Warrior II was recorded during ground runs. A set of temporarily attached accelerometers was used to record the response of the wing and the signals were recorded. Subsequently a Frequency Response Function was generated in the post-processing stage, which resulted in determining the first and second bending modes as well as the first twisting mode. A Finite Elements Model was applied to validate the results. Due to the limitations of the taxiing speed the method cannot excite higher frequency modes; however the findings can find numerous applications in real time in-flight flexure monitoring. | en_US |
dc.identifier.uri | http://hdl.handle.net/1959.4/10946 | |
dc.language | English | |
dc.language.iso | EN | en_US |
dc.publisher | The Institution of Engineers, Australia; The Royal Aeronautical Society, Australian Division | en_US |
dc.rights | CC BY-NC-ND 3.0 | en_US |
dc.rights.uri | https://creativecommons.org/licenses/by-nc-nd/3.0/au/ | en_US |
dc.source | Legacy MARC | en_US |
dc.subject.other | operational deflection shapes | en_US |
dc.subject.other | wing flexure | en_US |
dc.subject.other | modal frequency | en_US |
dc.subject.other | frequency analysis | en_US |
dc.subject.other | wing bending | en_US |
dc.subject.other | wing twisting | en_US |
dc.title | Modal Parameters of Light Aircraft Wing | en_US |
dc.type | Conference Paper | en |
dcterms.accessRights | open access | |
dspace.entity.type | Publication | en_US |
unsw.accessRights.uri | https://purl.org/coar/access_right/c_abf2 | |
unsw.identifier.doi | https://doi.org/10.26190/unsworks/86 | |
unsw.relation.faculty | Engineering | |
unsw.relation.ispartofconferenceLocation | Melbourne, Australia | en_US |
unsw.relation.ispartofconferenceName | Eleventh Australian International Aerospace Congress | en_US |
unsw.relation.ispartofconferenceProceedingsTitle | Proceedings of the Eleventh Australian International Aerospace Congress | en_US |
unsw.relation.ispartofconferenceYear | 2005 | en_US |
unsw.relation.originalPublicationAffiliation | Vulovic, Zoran, Mechanical & Manufacturing Engineering, Faculty of Engineering, UNSW | en_US |
unsw.relation.school | School of Mechanical and Manufacturing Engineering | * |
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