Multi-Fidelity Construction of Explicit Boundaries: Application to Aeroelasticity
Wings, control surfaces and rotor blades subject to aerodynamic forces may exhibit aeroelastic instabilities such as flutter, divergence and limit cycle oscillations which generally reduce their life and functionality. This possibility of instability must be taken into account during the design proc...
| Main Author: | |
|---|---|
| Other Authors: | |
| Language: | en |
| Published: |
The University of Arizona.
2013
|
| Subjects: | |
| Online Access: | http://hdl.handle.net/10150/293482 |