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Resources/Whitepapers/a5417e9d-64a1-4dd6-84f4-348232ecb474_FE Modeling Methodology for Load Analysis and Preliminary Sizing of Aircraft Wing Structure.pdf
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FE Modeling Methodology for Load Analysis and Preliminary Sizing of Aircraft Wing Structure
The finite element model has a direct impact on time and cost of analysis especially for internal load evaluation and initial sizing of the aircraft which constructed with enormous number of structural elements.
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