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. 2022 Nov 2;7(45):40701–40723. doi: 10.1021/acsomega.2c05930

Figure 12.

Figure 12

(a) Wing of an unmanned aerial vehicle with a morphing flap at the trailing edge capable of changing the deformation angle between (b) 39° and (c) 32°. The actuation mechanism is through resistive heating of both the SMA wires and the SMP–nichrome composite. (Reprinted from ref (165), with permission from Elsevier.)