A harmonic balance approach for modeling nonlinear aeroelastic behavior of wings in transonic viscous flow
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.
- Thomas, JP; Hall, KC; Dowell, EH
- January 1, 2003
- 44th Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics, and Materials Conference
International Standard Book Number 13 (ISBN-13)
Digital Object Identifier (DOI)