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Graphite-epoxy Composite Design for Aircrcaft Wing Spar Using Computational Techniques – Part I

by AKINDAPO Jacob Olaitan, JOHNSON-ANAMEMENA Nnaemeka and GARBA Danladi King

American Journal of Mechanical Engineering. 2017, 5(4), 117-127. DOI: 10.12691/ajme-5-4-2
Pub. Date: June 27, 2017Views: 49710 Downloads: 47934Like: 5

aircraft wing spar computational technique Finite Element Analysis (FEA) graphite-epoxy design shear force and bending moment

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