Vibrations of a High-Aspect-Ratio, Multi-Element Wing

Research output: Chapter in Book/Report/Conference proceedingConference contribution

1 Scopus citations

Abstract

A full-scale finite element model of a high aspect ratio, back swept, slotted-natural-laminar-flow wing is used to: 1) study the uncoupled and coupled modes of the two elements of the wing; 2) investigate the effects of connection stiffness and number of connections on the coupled modes. The two elements are attached via constraint equations and springs or connectors, using a component mode synthesis approach. The wing model includes the aerodynamic skins as well as internal structural elements. The analysis shows that increasing the stiffness of the springs can couple the two wings such that the low order modes resemble those of a conventional wing. Out-of-plane modes are the most compliant modes with coupling. Torsional modes become mixed bending/torsional modes, with the aft element undergoing most of the deformation. In-plane bending modes appear to evolve to mixed in-plane /out-of-plane/ torsion modes with more connectors or higher stiffness.

Original languageEnglish (US)
Title of host publicationAIAA SciTech Forum 2022
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624106316
DOIs
StatePublished - 2022
EventAIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022 - San Diego, United States
Duration: Jan 3 2022Jan 7 2022

Publication series

NameAIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022

Conference

ConferenceAIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
Country/TerritoryUnited States
CitySan Diego
Period1/3/221/7/22

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering

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