Journal of the Korean Society for Aeronautical & Space Sciences (한국항공우주학회지)

The Korean Society for Aeronautical and Space Sciences (한국항공우주학회)
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Analysis of Wrinkling for Creased Thin Membrane

접힌 자국이 있는 멤브레인의 주름 거동 해석

  • Published : 2008.09.04
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Abstract

In this paper, the wrinkling behavior of vertically creased corner-loaded square membranes was studied using geometrically nonlinear post-buckling analysis. The membranes were modeled using shell elements, and the meshes were seeded with semi-random geometrical imperfection to instigate the buckling deformation. A pristine and creased membranes with various initial deployment angles were considered in the analyses and the results were compared. Results showed that local wrinkles initiated near the corner where the higher load was applied, which grew to form a single diagonal global wrinkle as the load ratio increased. It was also found that the local wrinkle initiation and the global wrinkle formation were significantly dependent on the initial deployment angles.

본 논문에서는 수직방향으로 접은 사각형 멤브레인의 주름 거동을 기하학적 비선형 후좌굴 해석을 사용하여 연구하였다. 멤브레인은 쉘 요소로 모델링 하였고 하중은 멤브레인의 코너에서 대각선 방향으로 가하였다. 해석에는 다양한 각도의 초기 전개각을 가지는 멤브레인을 고려하였고 접힌 자국이 없는 경우에 대해서도 해석을 수행하여 그 결과를 비교하였다. 해석결과 주름은 큰 코너하중이 가해진 지역에서 국부적으로 발생하였는데, 이 국부 주름은 하중 비의 증가에 따라 점차 성장하여 전역 주름으로 발전하였다. 또한 주름의 발생 및 성장 거동은 접힌 자국의 초기 전개각에 좌우되는 경향을 보였다.

Keywords

References

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