33. Aeroelastic tailoring of high-aspect-ratio composite joined-wing UAV
Xiaomao Chen1, Jinglong Han2
State Key Lab of Mechanics and Control for
E-mail: firstname.lastname@example.org, email@example.com
Abstract. For the high-aspect-ratio composite joined-wing UAV, as the geometric nonlinear significant effect, nonlinear aeroelastic analysis method should be applied when study its aeroelastic tailoring method. In the paper, based on the secondary development of MSC/Nastran software with Direct matrix abstraction programme language, with the adopting the multidisciplinary design optimization platform Isight software integrating the MSC/Nastran software analysis, modules of the static aeroelastic analysis, nonlinear static analysis and flutter analysis, a nonlinear aeroelastic tailoring method for high –aspect-ratio composite joined-wing UAV has been presented. Example show that, the method proposed in this paper not only can solve nonlinear aeroelastic tailoring of high-aspect-ratio composite joined-wing UAV problem, but also can be applied to complex engineering structure.
Keywords: high-aspect-ratio, joined-wing UAV, aeroelastic tailoring, nonlinear.
 Wolkovitch J. The Joined Wing-An Overview. AIAA-1985-274, 1985.
 Weisshaar T. A., Lee D. H. Aeroelastic Tailoring of Joined-Wing Configurations. AIAA-2002-1207, 2002.
 Nonlinear Aeroelastic Analysis of Joined-Wing Aircraft with Fully Intrinsic Equations. AIAA‑2009‑2464, 2009.
 Dowell E., Edwards J., Strganac T. Nonlinear aeroelasticity. Journal of Aircraft, Vol. 40, 2003, p. 857‑874.
 Chen Quanlong, Han Jinglong, Yun Haiwei Flutter analysis of wings subjected to engine thrusts. Journal of Vibration Engineering, Vol. 25, Issue 2, 2012, p. 110‑116.
 Ran Yuguo, Han Jinglong, Yun Haiwei Development of aeroelastic response solution sequence with dmap language for freeplay nonlinear structure. Journal of Nanjing University of Aeronautics and Astronautics, Vol. 39, Issue 1, 2007, p. 41‑46.
 Xie Changchuan, Wu Zhigang, Yang Chao Aeroelastic analysis of flexible large aspect ratio wing. Journal of Beijing University of Aeronautics and Astronautics, Vol. 29, Issue 12, 2003.
 Shirk M. H., Hertz T. J., Weisshaar T. A. Aeroelastic tailoring-theory, practice and promise. Journal of Aircraft, Vol. 986, Issue 23, 1, p. 6‑18.
 Zhou Congqing Mechanism and benefit of the aeroelastic tailoring. Acta Materiae Compositae Sinica, Vol. 6, Issue 4, 1989, p. 1‑9.
 Weisshaar T. A., Nam C., Batista R. A. Aeroelastic Tailoring for Improved UAV Performance. AIAA-98-1757, NewYork, 1998.
 Dillinger J. K. S., Klimmek T., Abdalla M. M., Gürdal Z. Stiffness optimization of composite wing with aeroelastic constraints. Journal of Aircraft, Vol. 50, Issue 4, 2013, p. 1159‑1168.
 Zhou Lei, Wan Zhiqiang, Yang Chao Effect of laminate parameters of composite skin on aeroelastic optimization of high-aspect-ratio wing. Acta Materiae Compositae Sinica, Vol. 30, Issue 5, 2013, p. 195‑200.
 Liu Xiangning, Xiang Jinwu Study of aeroelastic tailoring of high-aspect ratio flexible composite wing. Journal of Beijing University of Aeronautics and Astronautics, Vol. 32, Issue 12, 2006, p. 1403‑1407.
 Li Chunming Optimization Method. Southeast University Press, Nanjing, 2009.
 Zhang Shujun, Wang Yuntao, Meng Dehong Study on static aeroelasticity for high-aspect-ratio joined-wings. Acta Aerodynamica Sinica, Vol. 32, Issue 2, 2013, p. 170‑174.
Cite this article
Chen Xiaomao, Han Jinglong Aeroelastic tailoring of high‑aspect-ratio composite joined‑wing UAV. Mathematical Models in Engineering, Vol. 3, Issue 1, 2017, p. 41‑48.
Mathematical Models in Engineering. June 2017, Volume 3, Issue 1
© JVE International Ltd. ISSN Print 2351-5279, ISSN Online 2424-4627, Kaunas, Lithuania