Kaygan, ErdoğanKöroğlu, Aslıhan TuğçeBaşak, Melisa2023-08-052023-08-052022 EylülKaygan, E., Köroğlu, A. T., Başak, M., (2022). Aerodynamic Efficiency Analysis of Variable Morphing Wings. International Journal of Aeronautics and Astronautics, 3(2), 71-86. DOI: 10.55212/ijaa.10883992757-6574https://hdl.handle.net/20.500.12395/49166In this paper, variable wing and/or winglet concepts are investigated. The impetus for the work was to identify and optimize wing and winglets to enhance the aerodynamic efficiency of a morphing aircraft. The analysis is based on changing sweep angle and wing-tip twist together with cant angle morphing (? = 0° - 45° ? = ?10°- 10° and ? = 0° - 30°). A variety of cases are examined through an aerodynamic analysis tool (VLM) comparing with baseline sweep wing configuration. As a result, significant improvements in flight characteristics are observed by adapting the required angle to receive optimum performance benefits.en10.55212/ijaa.1088399info:eu-repo/semantics/openAccessAerodynamicsDragMorphingSweepTwistArticle327186