Limit Cycle Oscillation and Domain of Stability in Prototypical Wing Sections with Unsteady Aerodynamics

Authors

Sushma Gujjula, University of Nevada, Las Vegas
Sahjendra N. Singh, University of Nevada, Las VegasFollow
Woosoon Yim, University of Nevada, Las VegasFollow

Document Type

Conference Proceeding

Publication Date

8-16-2004

Publication Title

Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference

Publisher

AIAA

First page number:

1180

Last page number:

1194

Keywords

Aeroelasticity; Flutter (Aerodynamics); Oscillations; Pitching (Aerodynamics); Unsteady flow (Aerodynamics)

Disciplines

Aeronautical Vehicles | Aerospace Engineering | Controls and Control Theory | Electrical and Electronics

Language

English

Comments

Conference held: August 16-18, 2004, Providence, Rhode Island

Permissions

Use Find in Your Library, contact the author, or interlibrary loan to garner a copy of the item. Publisher policy does not allow archiving the final published version. If a post-print (author's peer-reviewed manuscript) is allowed and available, or publisher policy changes, the item will be deposited.

Repository Citation

Gujjula, S., Singh, S. N., Yim, W. (2004). Limit Cycle Oscillation and Domain of Stability in Prototypical Wing Sections with Unsteady Aerodynamics. Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference 1180-1194. AIAA.