초기 비틀림이 있는 회전하는 복합재료 블레이드의 진동특성에 대한 연구

Vibration Characteristics of Rotating Composite Blades with Initial Twist

  • 기영중 (서울대학교 기계항공공학부 항공우주공학전공) ;
  • 김지환 (서울대학교 기계항공공학부)
  • 발행 : 2002.05.01

초록

Vibration analysis of rotating blade is the main purpose of the present study. In this study, general formulation is performed for rotating shell structures including the centrifugal force, Coriolis acceleration and initial twist. Furthermore, simplified equations are derived for the case of an open cylindrical shell. Based on the concept of degenerated shell element with the Reisser-Mindlin's assumptions, the finite element method is adopted for solving the problems. In addition, it is investigated the effect of the stacking sequence of the composites on the vibration characteristics of the blade. The results are summarized for the various parameters such as the speed of rotation and pre-twist of the blade. Also, present results are compared with the previous works and experimental data.

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