Transonic aeroelastic instability suppression for a swept wing by targeted energy transfer

Sean A. Hubbard, Raymond L. Fontenot, D. Michael McFarland, Paul G.A. Cizmas, Lawrence A. Bergman, Thomas W. Strganac, Alexander F. Vakakis

Research output: Contribution to journalArticle

Abstract

Targeted energy transfer is studied as a means for suppression of transonic aeroelastic instabilities of a wind-tunnel swept wing, with a focus on designing a lightweight nonlinear energy sink that improves the critical flutter condition. The aeroelastic response modes of the wing with a nonlinear energy sink coupled to the tip are identified and tested for robustness using a medium-fidelity computational aeroelasticity model, and confirm that robust suppression of transonic aeroelastic instabilities is achievable. Accordingly, a nonlinear energy sink is designed based on a parametric study, and its transonic aeroelastic effects are studied using medium- and high-fidelity models. The results of both models indicate an improvement in stability over a broad range of conditions; the high-fidelity model predicts an approximately 40% increase in the dynamic pressure at the critical stability condition. Finally, a prototype winglet-mounted nonlinear energy sink is modeled to examine its aeroelastic effects. The results show that the nonlinear-energy-sink design is robust, but the winglet design plays a critical role that must be considered in the overall effect.

Original languageEnglish (US)
Pages (from-to)1467-1482
Number of pages16
JournalJournal of Aircraft
Volume51
Issue number5
DOIs
StatePublished - Sep 1 2014

ASJC Scopus subject areas

  • Aerospace Engineering

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  • Cite this

    Hubbard, S. A., Fontenot, R. L., McFarland, D. M., Cizmas, P. G. A., Bergman, L. A., Strganac, T. W., & Vakakis, A. F. (2014). Transonic aeroelastic instability suppression for a swept wing by targeted energy transfer. Journal of Aircraft, 51(5), 1467-1482. https://doi.org/10.2514/1.C032339