北京航空航天大学学报 ›› 1999, Vol. 25 ›› Issue (2): 171-175.

• 论文 • 上一篇    下一篇

主动气动弹性机翼技术分析

杨超, 陈桂彬, 邹丛青   

  1. 北京航空航天大学 飞行器设计与应用力学系
  • 收稿日期:1997-10-07 出版日期:1999-02-28 发布日期:2010-09-28
  • 作者简介:男 31岁 讲师 100083 北京
  • 基金资助:

    航空科学基金(97A51038)资助项目

Analysis of Active Aeroelastic Wing Technology

Yang Chao, Chen Guibin, Zou Congqing   

  1. Beijing University of Aeronautics and Astronautics,Dept. of Flight Vehicle Design and Applied Mechanics
  • Received:1997-10-07 Online:1999-02-28 Published:2010-09-28

摘要: 以伺服气动弹性(或称气动伺服弹性)技术为出发点,结合国内外研究情况,分析近年来正在发展的、能多方面提高飞机性能的飞机设计新技术——主动气动弹性机翼(也称主动柔性机翼)技术的主要设计思想与特点、关键技术、与传统机翼设计技术的区别、应用前景等,反映该技术的多学科综合和一体化的特点,供飞机设计、气动弹性等研究人员参考.

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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