Modeling limit cycle oscillation behavior of the F-16 fighter using a harmonic balance approach
Publication
, Conference
Thomas, JP; Dowell, EH; Hall, KC; Denegri, CM
Published in: Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
December 1, 2004
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 Scholars
Published In
Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
ISSN
0273-4508
Publication Date
December 1, 2004
Volume
3
Start / End Page
2044 / 2050
Citation
APA
Chicago
ICMJE
MLA
NLM
Thomas, J. P., Dowell, E. H., Hall, K. C., & Denegri, C. M. (2004). Modeling limit cycle oscillation behavior of the F-16 fighter using a harmonic balance approach. In Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference (Vol. 3, pp. 2044–2050).
Thomas, J. P., E. H. Dowell, K. C. Hall, and C. M. Denegri. “Modeling limit cycle oscillation behavior of the F-16 fighter using a harmonic balance approach.” In Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, 3:2044–50, 2004.
Thomas JP, Dowell EH, Hall KC, Denegri CM. Modeling limit cycle oscillation behavior of the F-16 fighter using a harmonic balance approach. In: Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. 2004. p. 2044–50.
Thomas, J. P., et al. “Modeling limit cycle oscillation behavior of the F-16 fighter using a harmonic balance approach.” Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, vol. 3, 2004, pp. 2044–50.
Thomas JP, Dowell EH, Hall KC, Denegri CM. Modeling limit cycle oscillation behavior of the F-16 fighter using a harmonic balance approach. Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. 2004. p. 2044–2050.
Published In
Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
ISSN
0273-4508
Publication Date
December 1, 2004
Volume
3
Start / End Page
2044 / 2050