Further investigation of 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 19, 2005
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 Scholars
Published In
Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
ISSN
0273-4508
Publication Date
December 19, 2005
Volume
3
Start / End Page
1457 / 1466
Citation
APA
Chicago
ICMJE
MLA
NLM
Thomas, J. P., Dowell, E. H., Hall, K. C., & Denegri, C. M. (2005). Further investigation of 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. 1457–1466).
Thomas, J. P., E. H. Dowell, K. C. Hall, and C. M. Denegri. “Further investigation of 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, 3:1457–66, 2005.
Thomas JP, Dowell EH, Hall KC, Denegri CM. Further investigation of 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. 2005. p. 1457–66.
Thomas, J. P., et al. “Further investigation of 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, 2005, pp. 1457–66.
Thomas JP, Dowell EH, Hall KC, Denegri CM. Further investigation of 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. 2005. p. 1457–1466.
Published In
Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
ISSN
0273-4508
Publication Date
December 19, 2005
Volume
3
Start / End Page
1457 / 1466