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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
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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