Nonlinear aeroelastic analysis of high aspect-ratio wings using the method of numerical continuation
This research explores the impact of kinematic structural nonlinearities on the dynamics of a highly deformable cantilevered wing. Two different theoretical formulations are presented and analysed for nonlinear behavior. The first formulation, which is more conventional, assumes zero equilibrias and...
| Main Author: | |
|---|---|
| Other Authors: | |
| Format: | Others |
| Language: | en_US |
| Published: |
Texas A&M University
2006
|
| Subjects: | |
| Online Access: | http://hdl.handle.net/1969.1/3846 |