Agile Wing Integration - Nonlinear devices on a strut for loads control

Engineering

1. Gust Loads 100%
2. Beam Model 33%
3. Load Control 33%
4. Nonlinear Device 33%
5. Structural Model 33%
6. Geometric Nonlinearity 33%
7. Peak Load 27%
8. Aerospace Applications 27%
9. Stress Level 25%
10. NASA 25%
11. Joints (Structural Components) 25%
12. Damping Coefficient 25%