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Modeling of Triangular Lattice Space Structures with Curved BattensTechniques for simulating an assembly process of lattice structures with curved battens were developed. The shape of the curved battens, the tension in the diagonals, and the compression in the battens were predicted for the assembled model. To be able to perform the assembly simulation, a cable-pulley element was implemented, and geometrically nonlinear finite element analyses were performed. Three types of finite element models were created from assembled lattice structures for studying the effects of design and modeling variations on the load carrying capability. Discrepancies in the predictions from these models were discussed. The effects of diagonal constraint failure were also studied.
Document ID
20050175877
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Chen, Tzikang
(Army Research Lab. Hampton, VA, United States)
Wang, John T.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2005
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA Paper 2005-1967
Report Number: AIAA Paper 2005-1967
Meeting Information
Meeting: 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
Location: Austin, TX
Country: United States
Start Date: April 18, 2005
End Date: April 21, 2005
Sponsors: American Inst. of Aeronautics and Astronautics, American Society of Mechanical Engineers, American Society of Civil Engineers, American Helicopter Society, Inc., American Society for Composites
Funding Number(s)
WBS: WBS 23-817-10-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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