Finite Element Method Analysis and Experiment of 2-Dimensional Deployable Membrane Structures Embedding Inflatable Tubes

  • Kei Senda, Naoko Kishimoto, Ken Higuchi, Tomoyuki Oda, Tadashi Hattori
  • April 2008, American Institute of Aeronautics and Astronautics (AIAA)
  • DOI: 10.2514/6.2008-2054

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The following have contributed to this page: Dr. Kei Senda