2016
DOI: 10.1017/aer.2015.12
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On the wing density and the inflation factor of aircraft

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(1 citation statement)
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“…In such a design, a standard tail geometry is replaced by a trailing edge flap that converts the fuselage into a lifting body. [20][21][22] We designed, fabricated, and tested a UAV with morphing wings and a tail enabled by electrolaminate technology. Key features of the final optimized UAV design (shown in Figure 5) included: variable wingspan of 1.2-2.4 m with a corresponding change in wing area of nearly a factor of four; no vertical tail; a horizontal tail area variable by a factor of three; stability in all three axes; all actuation mechanisms (battery, engine etc.)…”
Section: Examples Of Application To Uavsmentioning
confidence: 99%
“…In such a design, a standard tail geometry is replaced by a trailing edge flap that converts the fuselage into a lifting body. [20][21][22] We designed, fabricated, and tested a UAV with morphing wings and a tail enabled by electrolaminate technology. Key features of the final optimized UAV design (shown in Figure 5) included: variable wingspan of 1.2-2.4 m with a corresponding change in wing area of nearly a factor of four; no vertical tail; a horizontal tail area variable by a factor of three; stability in all three axes; all actuation mechanisms (battery, engine etc.)…”
Section: Examples Of Application To Uavsmentioning
confidence: 99%