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

Dowell, Earl H.
Hall, Kenneth C.
Thomas, Jeffrey P.

Cited Authors

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

Published Date

December 1, 2004

Published In

Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference

Volume / Issue

Start / End Page

2044 - 2050

International Standard Serial Number (ISSN)

0273-4508

Citation Source

Scopus