A REVIEW ON APPLICATIONS AND EFFECTS OF MORPHING WING TECHNOLOGY ON UAVS
Abstract
Keywords
References
- Abdulrahim, M. (2003, March). Flight dynamics and control of an aircraft with segmented control surfaces. In 42nd AIAA Aerospace Sciences Meeting and Exhibit (p. 128).
- Abdulrahim, M., & Cocquyt, J. (2002, April). Development of Mission capable Flexible-Wing Micro Air Vehicles. In 53rd Southeastern Regional Student Conference.
- Abdulrahim, M., & Lind, R. (2004, August). Flight testing and response characteristics of a morphing gull-wing morphing aircraft. In AIAA guidance, navigation, and control conference and exhibit (p. 5113).
- Ajaj, R. M., & Jankee, G. K. (2018). The Transformer aircraft: A multimission unmanned aerial vehicle capable of symmetric and asymmetric span morphing. Aerospace Science and Technology, 76, 512-522.
- Bourdin, P., Gatto, A., & Friswell, M. (2006, June). The application of morphing cant angle winglets for morphing aircraft control. In 24th AIAA applied aerodynamics conference (p. 3660).
- Cadogan, D., Smith, T., Uhelsky, F., & Mackusick, M. (2004, April). Morphing inflatable wing development for compact package unmanned aerial vehicles.
- Dayyani, I., Shaw, A. D., Flores, E. S., & Friswell, M. I. (2015). The mechanics of composite corrugated structures: a review with applications in morphing aircraft. Composite Structures, 133, 358-380.
- Gamboa, P., Aleixo, P., Vale, J., Lau, F., & Suleman, A. (2007). Design and testing of a morphing wing for an experimental UAV. Unıversity Of Beira Interior Covilha (Portugal).
Details
Primary Language
English
Subjects
Aerospace Engineering
Journal Section
Review
Authors
Cevdet Özel
This is me
Türkiye
Emre Özbek
*
Türkiye
Selcuk Ekici
0000-0002-7090-3243
Türkiye
Publication Date
September 10, 2020
Submission Date
June 14, 2020
Acceptance Date
September 4, 2020
Published in Issue
Year 2020 Volume: 01 Number: 01