Parametric study of flutter for an airfoil in inviscid transonic flow
Journal Article (Academic article)
A parametric study of flutter was conducted for an airfoil in inviscid transonic flow. An inviscid computational flow dynamic harmonic balance aerodynamic-Euler-based code was used for the investigation. The computational efficiency of the time-linearized option of the harmonic balance aerodynamic model allows a much more thorough exploration of the parameter range than was previously achieved.
Duke Authors
Cited Authors
- Kholodar Denis, B; Thomas Jeffrey, P; Dowell Earl, H; Hall Kenneth, C
Published Date
- 2003
Published In
- Journal of Aircraft
Volume / Issue
- 40 / 2
Start / End Page
- 303 - 313