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This thesis explores single- and multiobjective design optimization applied to improving aircraft components. It introduces an aircraft component and aims to reduce its weight by 10% without reducing stiffness. This was not possible, so the goal was lowered to a 6.26% weight reduction while maintaining stiffness. The thesis covers preparing the component model, performing a sensitivity analysis, and single- and multiobjective optimizations using NX and modeFRONTIER software.

Author
Nirmalya Mishra
Language
EN

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