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Modelling and vibration of composite thin-walled rotating blades featuring extension-twist elastic coupling

机译:拉伸-扭转弹性耦合的复合薄壁旋转叶片的建模与振动

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摘要

The modelling and vibration of composite thin-walled pre-twisted rotating blades of non-uniform cross-sections along their span, and featuring the extension-twist elastic coupling are addressed. To this end, Hamilton's principle is used to derive the equations of motion and the associated boundary conditions. In addition to the pretwist and warping restraint, the exotic properties of advanced composite material are used, and the efficiency of implementing the tailoring technique toward the enhancement, without weight penalties, of the vibratory behaviour of rotating blades is illustrated. Comparisons between the predictions by both Wagner's and Washizu's approaches are presented, and pertinent conclusions regarding the implications of the various geometrical and physical characteristics of the blade are outlined.
机译:讨论了截面不均匀的复合薄壁预扭转旋转叶片沿其跨度的建模和振动,并具有延伸扭转弹性耦合。为此,使用汉密尔顿原理导出运动方程和相关的边界条件。除了预扭转和翘曲约束之外,还使用了高级复合材料的奇异特性,并说明了实施定制技术以提高旋转叶片的振动性能而无重量损失的效率。提出了Wagner方法和Washizu方法的预测结果之间的比较,并概述了有关叶片各种几何和物理特性的含义的相关结论。

著录项

  • 来源
    《The Aeronautical Journal》 |2005年第1095期|p.233-246|共14页
  • 作者

    S-Y. Oh; L. Librescu; O. Song;

  • 作者单位

    Department of Engineering Science and Mechanics Virginia Polytechnic Institute and State University Blacksburg, VA, USA;

  • 收录信息
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 航空;
  • 关键词

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