Damping Analysis of Pretwisted Composite Plates with Viscoelastic Layer

점탄성층을 갖는 비틀린 복합재판의 감쇠해석

  • 이덕규 (한국항공우주연구원 위성운영센터 위성응용연구그룹)
  • Published : 2002.10.01

Abstract

A three node triangular element with drilling rotations incorporating Improved Layerwise Zig-zag Theory(HZZT) is developed to analyze the vibration of spinning pretwisted composite blades with embedded damping layer. Matching conditions at the interfaces between the damping material and the border material are enforced by setting the shear forces matched and different shear strains along the interfaces. The natural frequencies and modal loss factors of cantilevered pretwisted composite blade with damping core are calculated with the present triangular element enforcing the matching conditions and compared to experimental results and MSC/NASTRAN results using a layered combination of plate and solid elements.

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