Modeling aerodynamic nonlinearities for two aeroelastic configurations: Delta wing and flapping flag

Journal Article

The flutter and LCO behavior of a delta wing and a flapping model were studied theoretically and the results were compared to experiment. Nonlinear aerodynamic and nonlinear structural theories were used in the theoretical modeling of the two aeroelastic systems. The resultant data were analyzed in detail.

Duke Authors

Cited Authors

  • Attar, PJ; Dowell, EH; Tang, D

Published Date

  • January 1, 2003

Published In

Volume / Issue

  • 1 /

Start / End Page

  • 12 - 22

International Standard Serial Number (ISSN)

  • 0273-4508

Citation Source

  • Scopus