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Bu makalede, ucak kontrolu ve performansi icin bukum cesitli kanat konfigurasyonlarinin etkinligi tanimlanmistir. Incelenen birincil degiskenler, ideal bir bukum acisini tanimlayarak, benzer bir Airbus A320 kanat yapisinin kanat bukulme acisinin degismesini icermektedir. Aerodinamik performans ve morphing kanadinin kontrolu AVL (Athena Vortex Lattice Method) ile cozumlenmistir. Farkli ucus rejimleri icin aerodinamik performansin ve bukum gecis kanadinin kontrolunun daha iyi anlasilmasi icin, onceden belirlenmis bukum degerleri (± 8 ° <ϕ <8 °, ± 2 ° adimlarla) incelenmistir. Bu calismadan elde edilen sonuclar, eger ucaklarda  bukulebilen kanatlar kullanilirsa, performans avantajlarinin elde edilebilecegini gostermektedir.

Effectiveness of Twist Morphing Wing on Aerodynamic Performance and Control of an Aircraft