Modeling limit cycle oscillation behavior of the F-16 fighter using a harmonic balance approach

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. Computed limit cycle response results correlate well with experiment. Details of the computational model and methodology are presented. Copyright © 2004 by Jeffrey P. Thomas, Earl H. Dowell, Kenneth C. Hall and Charles M. Denegri Jr.

Duke Authors

Cited Authors

  • Thomas, JP; Dowell, EH; Hall, KC; Jr, CMD

Published Date

  • 2004

Published In

Volume / Issue

  • 3 /

Start / End Page

  • 2044 - 2050

International Standard Serial Number (ISSN)

  • 0273-4508