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Volume 25 Issue 2
Feb.  1999
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Journal of Beijing University of Aeronautics and Astronautics  > 1999  >  25(2): 171-175.
Yang Chao, Chen Guibin, Zou Congqinget al. Analysis of Active Aeroelastic Wing Technology[J]. Journal of Beijing University of Aeronautics and Astronautics, 1999, 25(2): 171-175. (in Chinese)
Citation: Yang Chao, Chen Guibin, Zou Congqinget al. Analysis of Active Aeroelastic Wing Technology[J]. Journal of Beijing University of Aeronautics and Astronautics, 1999, 25(2): 171-175. (in Chinese)
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Analysis of Active Aeroelastic Wing Technology

  • Beijing University of Aeronautics and Astronautics,Dept. of Flight Vehicle Design and Applied Mechanics

  • Received Date: 07 Oct 1997
  • Publish Date: 28 Feb 1999
    Abstract
  • Based on aerosevorelasticity technology, active aeroelastic wing technology (also called active flexible wing technology) was discussed. Active aeroelastic wing technology was advanced technology of aircraft design to improve performance from a lot of cases. The main design concept and characteristic, key technology (mathematics model of aerosevorelasticity system, integrated design, analysis method for stability, and design of active control system), difference to classical wing design, and functions for future aircraft were analyzed. The design with integrated multidisciplinary in the technology was showed mainly and was important to the research person for future aircraft design.

     

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  • 1. Perry B, Cole S R, Miller G D. Summary of an active flexible wing program.J Aircraft,1995,32(1):10~15 2. Pendleton E, Griffin K E, Kehoe M W,et al. A flight research program for active aeroelastic wing technology. AIAA-96-1574-CP,1996 3. 邹丛青, 陈桂彬. 气动弹性力学的新分支——气动伺服弹性. 北京航空航天大学学报,1995,21(20):22~27 4. 陈桂彬,邹丛青. 基于气动能量概念的机翼颤振抑制控制律. 中国航空科技文献, HJB860356, 1986 5. 邹丛青,陈桂彬. 机翼／外挂颤振主动抑制的控制律研究. 力学学报,1991,23(3):274~281 6. 张芝龙. 颤振主动抑制系统综合与实验研究:[学位论文]. 北京:北京航空航天大学飞行器设计与应用力学系,1992 7. 方 力,陈桂彬. 颤振主动抑制控制律优化设计. 北京航空航天大学科研报告,BH-B4431,1993 8. 何景武,邹丛青. 颤振主动抑制系统鲁棒控制律初探. 北京航空航天大学学报,1995,21(2):10~15 9. 孙 卫,邹丛青. 耦合的气动弹性系统鲁棒稳定裕度估算. 北京航空航天大学学报,1996,22(3):386~393 10. 高 萍. 翼面结构／颤振主动控制一体化设计:[学位论文].北京:北京航空航天大学飞行器设计与应用力学系,1993 11. Miller G D. An active flexible wing multi-disciplinary design optimization method. AIAA-94-4412-CP,1994 12. 宗 捷. 非定常空气动力有理函数近似及非线性颤振研究:[学位论文].北京:北京航空航天大学飞行器设计与应用力学系,1995 13. 陈立新. 用于气动伺服弹性的低阶建模方法及其应用研究:[学位论文].北京:北京航空航天大学飞行器设计与应用力学系, 1997 14. Volk J A, Ausman J D, Tich E J. The role of automated multi-disciplinary structure sizing in flexible wing development. AIAA-94-1485,1994 15. Pendleton E, Lee M, Wasserman L. An application of the active flexible wing concept to an F-16 derivative wing model. AIAA-91-0987-CP,1991 16. 陆 波. 线性和带有非线性控制环节的气动伺服弹性稳定性分析:[学位论文]. 北京:北京航空航天大学飞行器设计与应用力学系,1997 17. 邹丛青,陈桂彬. 数字式颤振主动抑制及工程特性. 中国航空科技文献, HJB931162, 1993 18. Cheng P Y, Hirner T J. Automated procedures for aeroservorelastic compensation. AIAA-92-4606-CP, 1992
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