Nonlinear Dynamics and Control of Wings and Panels
Abstract
Experimental and theoretical studies of the nonlinear dynamics and control of aeroelastic systems including airfoils and wings have been conducted. Nonlinear geometric stiffness and freeplay have been considered specifically and good theoretical / experimental correlation obtained. Active control systems have been designed, built and tested to increase flutter speed and reduce limit cycle oscillations (LCO).
Document Details
- Document Type
- Technical Report
- Publication Date
- Nov 01, 2000
- Accession Number
- ADA388297
Entities
People
- Earl H. Dowell
- Lawrence N. Virgin
- Robert L. Clark Jr.
Organizations
- Duke University