Effects of Unbalanced Lamination Parameters on the Static Aeroelasticity of a High Aspect Ratio Wing

Figure 13

Displacement comparison in different directions in each laminated area.

(a) Leading edge longitudinal displacement in area I

(b) Leading edge longitudinal displacement in area II

(c) Leading edge longitudinal displacement in area III

(d) Leading edge wingspan displacement in area I

(e) Leading edge wingspan displacement in area II

(f) Leading edge wingspan displacement in area III

(g) Leading edge chord displacement in area I

(h) Leading edge chord displacement in area II

(i) Leading edge chord displacement in area III