A harmonic balance approach for modeling nonlinear aeroelastic behavior of wings in transonic viscous flow

Journal Article

Presented is a frequency-domain harmonic-balance (HB) computational fluid dynamic (CFD) approach for modeling flutter onset and limit cycle oscillation (LCO) behavior of viscous transonic aeroelastic wing configurations. The AGARD 445.6 transonic wing configuration is studied and results are compared to a recent inviscid analysis for a supersonic Mach number flow condition. © 2003 by Jeffrey P. Thomas, Kenneth C. Hall, and Earl H. Dowell. Published by the American Institute of Aeronautics and Astronautics, Inc.

Duke Authors

Cited Authors

  • Thomas, JP; Hall, KC; Dowell, EH

Published Date

  • December 1, 2003

Published In

  • 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference

Citation Source

  • Scopus