Further investigation of modeling limit cycle oscillation behavior of the F-16 fighter using a harmonic balance approach

Published

Conference Paper

A computational investigation of limit cycle oscillation behavior of the F-16 fighter configuration using a nonlinear frequency-domain harmonic-balance approach is presented. The research discussed in this latest paper is a follow-on to our work presented at the 2004 SDM conference. Our latest efforts have been directed toward assessing the effects of mean angle-of-attack, wingtip geometry, wing twist, and static aeroelastic deformation on flutter onset and LCO response.

Duke Authors

Cited Authors

  • Thomas, JP; Dowell, EH; Hall, KC; Denegri, CM

Published Date

  • December 19, 2005

Published In

Volume / Issue

  • 3 /

Start / End Page

  • 1457 - 1466

International Standard Serial Number (ISSN)

  • 0273-4508

Citation Source

  • Scopus