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Crease Behavior of Thin Membrane

멤브레인의 접힘 거동 연구

  • 우경식 (충북대학교 구조시스템공학과)
  • Published : 2007.10.31

Abstract

In this paper, geometrically and materially non-linear finite element analyses were performed to study the crease behavior of thin membranes. The cross-section of the membrane was modeled with 2-dimensional plane strain elements. To simulate the creasing process, the membrane mesh was folded, compressed to prescribed crease gauge by activating two rigid contact surfaces, and then released to give the crease topology. Various crease gauges were considered to investigate the effect of crease intensity on the initial deployment angle. The crease geometry was also obtained by experiments and the results were compared.

이 논문에서는 기하학적 및 재료적 비선형 유한요소해석을 통하여 멤브레인의 접힘 거동을 연구하였다. 얇은 멤브레인의 단면에 대해 평면변형률을 가정하여 2차원 요소로 모델링 하였다. 접힘 과정은 먼저 멤브레인 메쉬를 접은 후, 두 개의 강체 접촉면을 사용하여 지정된 접힘 간극까지 압축한 다음, 강체 접촉면을 풀어 접힘 형상을 얻는 순서로 모사하였다. 다양한 접힘 간극에 대해 해석을 수행하여 접힘 강도가 초기 전개각에 미치는 영향을 중심으로 결과를 고찰하였다. 또한 실제 시편에 대하여 실험을 수행하여 그 결과를 해석결과와 비교하였다.

Keywords

References

  1. Jenkins, C. H. (Ed.), Gossamer Spacecraft: Membrane and Inflatable Structures Technology for Space Application, AIAA, 2001
  2. Jenkins, C. H. (Ed.), Recent Advances in Gossamer Spacecraft, AIAA, 2006
  3. Miura, K, Method of Packaging and Deployment of Large Membranes in Space, International Astronautical Federation, Paper IAF-80-A31, Tokyo, Japan, 1980
  4. Murphey, T. W., A Nonlinear Elastic Constitutive Model for Wrinkled Thin Films, PhD. Dissertation, University of Colorado, 2000
  5. Horner, G. G. and Elliot, M. D., A Fabrication and Development Approach for a Miura-Ori Solar Sail Model, Proc. 43rd AIAA/ASME/ASCE/AHS/ACS SDM Conference, AIAA-2002-1702, Denver, CO, April 22-25, 2002
  6. Furuya, H., Inoue, Y. and Masuoka, T., Deployment Characteristics of Rotationally Skew Fold Membrane for Spinning Solar Sail, Proc. 46th AIAA/ASME/ASCE/AHS/ACS SDM Conference, AIAA-2005-2045, 18-21 April 2005, Austin, TX
  7. Miyazaki, Y. K, Furuya, H., Murata, S. and Takadama, K, Effects of Initial Configuration on Large Deformation Analysis for One-Dimensional Deployable Membrane, Proc. 46th AIAA/ASME/ASCE/AHS/ACS SDM Conference, AIAA-2005-2046, 18-21 April 2005, Austin, TX
  8. Papa, A. and Pellegrino, S., Mechanics of Systematically Creased Thin-Film Membrane Structures, Proc. 46th AIAA/ASME/ASCE/AHS/ACS SDM Conference, AIAA-2005-1975, 18-21 April 2005, Austin, TX
  9. Gough, A., Hossain, N. M. A., Jenkins, C. H., Blandino, J. and Hendricks, A., Experimental and Numerical Study of Creased Membranes, Proc. 46th AlAA/ASME/ASCE/AHS JACS SDM Conference, AIAA-2005-1976, 18-21 April 2005, Austin, TX
  10. Hossain, N. M. A., Woo, K. and Jenkins, C. H., Nonlinear Material Response of Systematically Creased Membranes, Proc. of 47th AIAA/ASME/ASCE/AHS/ACS SDM Conference, AIAA-2006-1801, 1-4 May 2006, Newport, RI
  11. Tessler, A., Sleight, D. W., and Wang, J. T., Effective Modeling and Nonlinear Shell Analysis of Thin Membranes Exhibiting Structural Wrinkling, Journal of Spacecraft and Rockets, Vol. 42, No. 2, pp. 287-298, 2005 https://doi.org/10.2514/1.3915
  12. Wong, Y. W., Pellegrino, S. and Park, K. C., Prediction of Wrinkle Amplitudes in Square Solar Sails, Proc. 44th AlAA/ASME/ASCE/AHS/JACS SDM Conference, AIAA-2003-1982, 2003
  13. Woo, K. and Jenkins, C. H., Global/Local Analysis Strategy for Partly Wrinkled Membrane, Journal of Spacecraft and Rockets,. Vol 43, No. 5., pp. 1101-1106, 2006 https://doi.org/10.2514/1.18603
  14. Miler, R. K., Hedgepeth, J. M., Weingarten, V. I., Das, P., and Kahyai, S., Finite Element Analysis of Partly Wrinkled Membranes, Computers and Structures, Vol. 20, Nos. 1-3, pp. 631-609, 1982 https://doi.org/10.1016/0045-7949(85)90111-7
  15. Roddeman, D. G., Finite-Element Analysis of Wrinkling Membranes, Communications in Applied Numerical Methods, Vol. 7, No. 4, pp. 299-307, 1991 https://doi.org/10.1002/cnm.1630070408
  16. Woo, K., lgawa, H. and Jenkins, C. H., Analysis of Wrinkling Behavior of Anisotropic Membrane, CMES: Computer Modeling in Engineering & Sciences, Vol. 6, No. 4, pp. 397-408, 2004
  17. MacNeal, R. and Robbins, E., Tensile Properties of a Tape with a Transverse Crease, Astro Research Corportation, ARC-R-241, 1967
  18. Murphy, D., Trautt, D., McEachen, M., Messener, D., Laue, G., and Gierow, P., Progress and Plans for System Demonstration of a Scalable Solar Sail, Proc. of 14th AAS/AIAA Space Flight Mechanics Conference, 8-12 Feb 2004, Maui, HI