A harmonic balance approach for modeling nonlinear aeroelastic behavior of wings in transonic viscous flow
Conference Paper
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.
Duke Authors
Cited Authors
- Thomas, JP; Hall, KC; Dowell, EH
Published Date
- August 28, 2003
Published In
Volume / Issue
- 7 /
Start / End Page
- 4779 - 4784
International Standard Serial Number (ISSN)
- 0273-4508
Citation Source
- Scopus