- Thomas, Jeffrey P. and Dowell, Earl H. and Hall, Kenneth C. and Denegri Jr., Charles M., 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
pp. 1457 - 1466 .
(last updated on 2007/04/07)
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.
Fighter aircraft;Frequency domain analysis;Harmonic analysis;Wings;Flutter (aerodynamics);Aerodynamics;Computer simulation;