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What is Composite Wing Spar Structural Analysis about?

This document discusses the structural analysis and performance-based validation of composite wing spars for the NASA X-57 electric aircraft, focusing on the need for high aspect ratio wings to enhance operational range. It details the use of ply-based laminate finite element methods to assess the strength and load paths of the wing spars, aiming to reduce testing burdens and ensure safety. The study includes optimization techniques for scaling and stress analysis to improve the design and validation proces

Author

yijunjie

Language

EN