Derleme
Yıl 2020,
Cilt: 01 Sayı: 01, 30 - 40, 10.09.2020
Öz
Kaynakça
- 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).
- Hui, Z., Zhang, Y., & Chen, G. (2019). Aerodynamic performance investigation on a morphing unmanned aerial vehicle with bio-inspired discrete wing structures. Aerospace Science and Technology, 95, 105419.
- https://www.santacruzgalapagoscruise.com/experience-waved-albatrosses-galapagos
- Kuder, I. K., Arrieta, A. F., Raither, W. E., & Ermanni, P. (2013). Morphing stiffness material and structural concepts for morphing applications. Progress in Aerospace Sciences, 63, 33-55.
- Lee, S., Tjahjowidodo, T., Lee, H., & Lai, B. (2017). Investigation of a robust tendon-sheath mechanism for flexible membrane wing application in mini-UAV. Mechanical Systems and Signal Processing, 85, 252-266.
- Woods, B. K., & Friswell, M. I. (2015). The adaptive aspect ratio morphing wing: design concept and low fidelity skin optimization. Aerospace Science and Technology, 42, 209-217.
- Wu, M., Shi, Z., Xiao, T., & Ang, H. (2019). Energy optimization and investigation for Z-shaped sun-tracking morphing-wing solar-powered UAV. Aerospace Science and Technology, 91, 1-11.
- Zi, K. A. N., Daochun, L. I., XIANG, J., & CHENG, C. (2019). Delaying stall of morphing wing by periodic trailing-edge deflection. Chinese Journal of Aeronautics.
- AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference (p. 1807).
Yıl 2020,
Cilt: 01 Sayı: 01, 30 - 40, 10.09.2020
Öz
Unmanned aerial vehicles (UAVs) have excelled with their ability to perform the intended task on or without personnel. In recent years, UAVs have been designed for civilian purposes as well as military applications. Morphing wings are deformable wing applications developed as a result of the need of different lift and drag forces in various phases of the flight of aircraft. It is an application which enables altering the wing aspect ratio, wing airfoil, wing airfoil camber ratio, wing reference and even different angles of attack are obtained in different parts of the wing.
Althoughy morphing wing application has just begun on today’s UAVs, modern airliners already have morphing wingtip devices such as Boeing 777-X’s. The benefits of the use of morphing wings for UAVs make this technology important. UAVs with morphing wing technology; may increase its payload ratio, may achieve a shorter take-off distance, may land and stop in shorter distance, may take-off where runway clearence is limited, has more efficient altitude change at lower engine RPMs, can obtain higher cruise speeds, may decrease its stall speed, may lower its drag if necessary, thus; saving energy and time.
Anahtar Kelimeler
Kaynakça
- 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).
- Hui, Z., Zhang, Y., & Chen, G. (2019). Aerodynamic performance investigation on a morphing unmanned aerial vehicle with bio-inspired discrete wing structures. Aerospace Science and Technology, 95, 105419.
- https://www.santacruzgalapagoscruise.com/experience-waved-albatrosses-galapagos
- Kuder, I. K., Arrieta, A. F., Raither, W. E., & Ermanni, P. (2013). Morphing stiffness material and structural concepts for morphing applications. Progress in Aerospace Sciences, 63, 33-55.
- Lee, S., Tjahjowidodo, T., Lee, H., & Lai, B. (2017). Investigation of a robust tendon-sheath mechanism for flexible membrane wing application in mini-UAV. Mechanical Systems and Signal Processing, 85, 252-266.
- Woods, B. K., & Friswell, M. I. (2015). The adaptive aspect ratio morphing wing: design concept and low fidelity skin optimization. Aerospace Science and Technology, 42, 209-217.
- Wu, M., Shi, Z., Xiao, T., & Ang, H. (2019). Energy optimization and investigation for Z-shaped sun-tracking morphing-wing solar-powered UAV. Aerospace Science and Technology, 91, 1-11.
- Zi, K. A. N., Daochun, L. I., XIANG, J., & CHENG, C. (2019). Delaying stall of morphing wing by periodic trailing-edge deflection. Chinese Journal of Aeronautics.
- AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference (p. 1807).
Toplam 16 adet kaynakça vardır.
Ayrıntılar
| Birincil Dil | İngilizce |
|---|---|
| Konular | Uzay Mühendisliği |
| Bölüm | Review |
| Yazarlar | |
| Yayımlanma Tarihi | 10 Eylül 2020 |
| Gönderilme Tarihi | 14 Haziran 2020 |
| Yayımlandığı Sayı | Yıl 2020 Cilt: 01 Sayı: 01 |
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