Research Article

Multistrand, Fast Reaction, Shape Memory Alloy System for Uninhabited Aerial Vehicle Flight Control

Table 1


WingHorizontal
tail
Vertical
tail

Span66.5226in
Area65011040.5in2
MGC LE FS1238.533in
Aspect ratio6.84.40.9
Thickness ratio0.11
Total polyhedral angle8N/AN/A
Aileron chord ratio0.19N/AN/A
Aileron span ratio0.38N/AN/A
Root chord9.56.039.5in
Tip chord64.344.06in
Average chord$7.75$5.18$6.78in

Fuselage

Length47in
Maximum height1.91in
Minimum width2.17in