List of Tables

1. List of peak values of the load factor PA
2. Verolme panel geometry and material
3. Cylinder under torsion load: Eigenvalues λ.
4. Hexadome (Healey problem): Linear buckling analysis results.
5. Material properties
6. Computed eigenfrequencies
7. Input options
8. Eigenfrequencies
9. Analytical eigenfrequencies fi
10. Geometry
11. Material properties
12. Input options
13. Eigenfrequencies helicopter rotor
14. Deformation solutions for loading condition C1: Tip displacement in z direction, at y=0.
15. Piezoelectric beam actuator: Actuator loading results
16. Piezoelectric beam actuator: Sensor voltage results
17. Input options
18. Analytical results:Axial loading in x-direction
19. Analytical results:Axial loading in xy-direction
20. Analytical results: Bending around the x-axis
21. Analytical results:Bending around the y-axis
22. Nodal coordinates
23. Displacement function coefficients
24. Results with symmetric BC's
25. Results with anti-symmetric BC's
26. Input options
27. Results to be expected.
28. Laminate 1: symmetric cross-ply
29. Laminate 2: asymmetric cross-ply