DOI QR코드

DOI QR Code

Thermoelastic Behaviors of Fabric Membrane Structures

  • Roh, Jin-Ho (Department of Aerospace Engineering, Korea Advanced Institute of Science and Technology) ;
  • Lee, Han-Geol (P/T NVH Team, GM Daewoo Auto and Technology) ;
  • Lee, In (Department of Aerospace Engineering, Korea Advanced Institute of Science and Technology)
  • Published : 2008.12.01

Abstract

The thermoelastic behaviors of an inflatable fabric membrane structure for use in a stratospheric airship envelope are experimentally and numerically investigated. Mechanical tensile properties of the membrane material at room, high, and low temperatures are measured using an $Instron^{(R)}$ universal testing machine and an $Instron^{(R)}$ thermal chamber. To characterize the nonlinear behavior of the inflated membrane structure due to wrinkling, the bending behavior of an inflated cylindrical boom made of a fabric membrane is observed at various pressure levels. Moreover, the envelope of a stratospheric airship is numerically modeled based on the thermoelastic properties of the fabric membrane obtained from experimental data, and the wrinkled deformed shape induced by a thermal load is analyzed.

Keywords

References

  1. A. Nayler, Airship activity and development world-wide-2003, AIAA's 3rd Aviation Technology, Integration and Operations (ATIO) Technical Forum, Denver, CO, USA (2003).
  2. Y.-G. Lee, D.-M. Kim and C.-H. Yeom, Development of Korea high altitude platform systems, Intl J. Wireless Info. Networks 13, 31-42 (2006). https://doi.org/10.1007/s10776-005-0018-6
  3. C. M. Jenkins, Gossamer spacecraft: membrane and inflatable structures technology for space applications, Progress in Astronautics and Aeronautics, Vol. 191, American Institute of Aeronautics and Astronautics, USA (2000).
  4. J. R. Blandino, J. D. Johnston, J. J. Miles and U. K. Dharamsi, The effect of asymmetric mechanical and thermal loading on membrane wrinkling, Proc. 43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Denver, CO, USA (2002).
  5. E.-J. Yoo, J.-H. Roh and J.-H. Han, Wrinkling control of inflatable booms using shape memory alloy wires, Smart Mater. Struct. 16, 340-348 (2007). https://doi.org/10.1088/0964-1726/16/2/012
  6. M. Stein and J. M. Hedgepeth, Analysis of partly wrinkled membranes, Technical Note, NASA TN D-813 (1961).
  7. S. Kang and S. Im, Finite element analysis of dynamic responses of wrinkling membranes, Comput. Methods Appl. Mech. Engng 173, 227-240 (1999). https://doi.org/10.1016/S0045-7825(98)00271-0