Decamber Morphing Concepts by Using a Hybrid Trailing Edge Control Surface
AbstractThe idea of morphing is drawing extensive attention in aerospace technologies. Several different approaches like span, camber, twist, and sweep are finding applications. In this work, the concept of a trailing edge control surface which is capable of performing decamber morphing is explained. The upper and lower parts of the control surface undergo different chordwise elongations and the difference between these displacements gives rise to either camber or decamber morphing. The necessary force is achieved by the help of servo actuators. During the design, the structural analyses were done to determine the best viable options for the number of servo actuators, the location of the servo actuators, and the material properties used in the control surface. The control surface was designed of aluminum, composite and compliant materials hence was called a hybrid one. The structural analyses were conducted by using ANSYS® Workbench v14.0 package program. After finding the best viable design, which was made for in vacuo condition, the proposed design was also verified under the simulated aerodynamic loading. The aerodynamic loads were obtained from CFD analyses which were done with SU2 V3.2.3 open-source flow solver. View Full-Text
Share & Cite This Article
Yaman, Y.; Tunçöz, İ.O.; Yang, Y.; Arslan, P.; Kalkan, U.; Tıraş, H.; Gürses, E.; Şahin, M.; Özgen, S. Decamber Morphing Concepts by Using a Hybrid Trailing Edge Control Surface. Aerospace 2015, 2, 482-504.
Yaman Y, Tunçöz İO, Yang Y, Arslan P, Kalkan U, Tıraş H, Gürses E, Şahin M, Özgen S. Decamber Morphing Concepts by Using a Hybrid Trailing Edge Control Surface. Aerospace. 2015; 2(3):482-504.Chicago/Turabian Style
Yaman, Yavuz; Tunçöz, İlhan O.; Yang, Yosheph; Arslan, Pınar; Kalkan, Uğur; Tıraş, Harun; Gürses, Ercan; Şahin, Melin; Özgen, Serkan. 2015. "Decamber Morphing Concepts by Using a Hybrid Trailing Edge Control Surface." Aerospace 2, no. 3: 482-504.