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FE modeling of Satellite’s Honeycomb Sandwich Panels Using Shell Approach and Solid Approach

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FE modeling of honeycomb sandwich panels used in the primary structure of satellite’s structure can be developed using both approaches proposed in this paper.

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This page is a summary of: FE modeling of Satellite’s Honeycomb Sandwich Panels Using Shell Approach and Solid Approach, September 2017, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/6.2017-5184.
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