Research Article

[Retracted] Application and Optimization of Wing Structure Design of DF-2 Light Sports Aircraft Based on Composite Material Characteristics

Table 4

The height record of the root and tip of the wing at both ends of the wing during the test.

LoadLeft wing tip heightLeft root heightLeft wing differenceRight wing tip height

10% load253.98214.4639.52241.8
20% load267.9216.8851.02245.28
30% load273.6218.5455.06254.22
40% load275.5211.5663.94256.2
50% load284.68212.871.88258.42
60% load291.62214.5877.04265.00
70% load294.00208.4685.54268.38
80% load299.02208.2890.74272.82