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

Table 2

Test protocol and results.

Test number	/mm	/mm	Wing tip deformation/mm	Maximum stress/MPa
1	320	190	19.551	184.11
2	280	190	11.836	126.1
3	360	190	11.92	122.07
4	320	223	23.011	173.84
5	280	223	15.327	121.21
6	360	223	16.614	101.76
7	320	256	22.55	183.54
8	280	256	13.633	76.959
9	360	256	15.613	91.109