Aerodynamic Efficiency Analysis of Variable Morphing Wings
Yükleniyor...
Dosyalar
Tarih
2022 Eylül
Dergi Başlığı
Dergi ISSN
Cilt Başlığı
Yayıncı
Selçuk Üniversitesi
Erişim Hakkı
info:eu-repo/semantics/openAccess
Özet
In 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.
Açıklama
Anahtar Kelimeler
Aerodynamics, Drag, Morphing, Sweep, Twist
Kaynak
International Journal of Aeronautics and Astronautics
WoS Q Değeri
Scopus Q Değeri
Cilt
3
Sayı
2
Künye
Kaygan, 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.1088399
