10-4. Aeroelastic Optimization
Learning from bionic lift and thrust mechanisms, modelled by generic morphing geometry
Test cases for aeroelastic flutter control by coupled wing motion and section morphing
Test configuration X-56: An active flutter control UAV |
Surface geometry model for aeroelastic analysis using geometrical surface morphing |
Parametric generation of wing flapping / flutter geometry coupled with distributed section control |
Aeroelastic surface deformations: animation |
