|
|
- 2015
采用等效有限元模型的复合材料机翼结构优化
|
Abstract:
| [1] | Zhao Q. Research on the layout optimization design method of composite wing structures[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2010 (in Chinese). 赵群. 复合材料翼面结构布局优化设计方法研究[D]. 南京: 南京航空航天大学, 2010. |
| [2] | Jones R M. Mechanics of composite materials[M]. 2nd ed. Philadelphia: Taylor & Francis Inc, 1999: 55-118. |
| [3] | Collier, Research, Corporation. HyperSizer Pro User Manual[M]. Newport News, Virginia: Collier Research Corporation, 2008: 119-121. |
| [4] | Kasapoglou C. Design and analysis of composite structures with application to aerospace structures[M]. Chichester: John Wiley & Sons, Ltd, 2010:132-138. |
| [5] | Chinese Aeronautical Establishment. Guide of composite buckling analysis[M]. Beijing: Aviation Industry Press, 2002: 5-9 (in Chinese). 中国航空研究院. 复合材料结构稳定性指南[M]. 北京: 航空工业出版社, 2002: 5-9. |
| [6] | Niu M C Y. Airframe structural design[M]. Hong Kong: Conmilit Press Ltd, 1995: 134-137. |
| [7] | Kulfan B M. A universal parametric geometry representation method-CST, AIAA-2007-0062[R]. Reston: AIAA, 2007. |
| [8] | Wan Z Q, Yang C. Aeroelastic optimization of a high-aspect-ratio composite wing[J]. Acta Materiae Compositae Sinica, 2005, 22(3): 145-149 (in Chinese). 万志强, 杨超. 大展弦比复合材料机翼气动弹性优化[J]. 复合材料学报, 2005, 22(3): 145-149. |
| [9] | Li S H, Yang Z C, Gu Y S, et al. A different aeroelastic tailoring of a composite joined-wing[J]. Journal of Northwestern Polytechnical University, 2008, 26(3): 292-296 (in Chinese). 李少华, 杨智春, 谷迎松, 等. 复合材料连翼的气动弹性剪裁研究[J]. 西北工业大学学报, 2008, 26(3): 292-296. |
| [10] | Weck O D, Agte J, Sobieszczanski-Sobieski J, et al. State-of-the-art and future trends in multidisciplinary design optimization, AIAA-2007-1905[R]. Reston: AIAA, 2007. |
| [11] | Xie C C, Zhang X, Chen G B. Dynamic modeling and flutter analysis for high-aspect-ratio composite wing[J]. Aircraft Design, 2004(2): 6-10 (in Chinese). 谢长川, 张欣, 陈桂彬. 复合材料大展弦比机翼动力学建模与颤振分析[J]. 飞机设计, 2004(2): 6-10. |
| [12] | Jin H B. Study on the system of composite synthesis optimization for aircraft structures[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2003 (in Chinese). 金海波. 复合材料飞机结构综合优化设计系统研究[D]. 南京: 南京航空航天大学, 2003. |
| [13] | Xiao Z P, Zhao Q, Xu J F. Optimization design of composite strut-braced wings with aeroelastic constraint[J]. Acta Materiae Compositae Sinica, 2014, 31(1): 194-199 (in Chinese). 肖志鹏, 赵群, 徐吉峰. 考虑气动弹性约束的复合材料支撑机翼优化设计[J]. 复合材料学报. 2014, 31(1): 194-199. |
| [14] | Bradley K R. A sizing methodology for the conceptual design of blended-wing-body transports[D]. Washington: George Washington University, 2004. |
| [15] | Ouyang X, Yu X Q, Wang Y. Flutter analysis for wing structure using finite element modeling with equivalent stiffness[J]. Journal of Vibroengineering, 2014, 16(3): 1483-1493. |
| [16] | Wenzel J, Sinapius M, Gabbert U. Primary structure mass estimation in early phases of aircraft development using the finite element method[J]. CEAS Aeronautical Journal, 2012, 3(1): 35-44. |
| [17] | Weisshaar T A, Nam C, Batista R A. Aeroelastic tailoring for improved UAV performance, AIAA-1998-1757[R]. Reston: AIAA, 1998. |
| [18] | Zhang X, Wu Z G, Yang C. Dynamic and flutter analysis of long-straight-wing based on equivalent beam model[J]. Journal of Beijing University of Aeronautics and Astronautics, 2010, 36(11): 1373-1377 (in Chinese). 张旭, 吴志刚, 杨超. 基于等效梁模型的长直机翼动力学与颤振分析[J]. 北京航空航天大学学报, 2010, 36(11): 1373-1377. |
| [19] | Lee U. Equivalent continuum beam-rod models of aircraft wing structures for aeroelastic analysis, AIAA-1994-1695[R]. Reston: AIAA, 1994. |
| [20] | Wright J R, Cooper J E. Introduction to aircraft aeroelasticity and loads[M]. Chichester: John Wiley & Sons, Ltd, 2007: 427-436. |
| [21] | Stone S C, Henderson J L, Nazari M M, et al. Evaluation of equivalent laminated plate solution (ELAPS) in HSCT sizing, AIAA-2000-1452[R]. Reston: AIAA, 2000. |
