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2 results for computational technique.

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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: 22084Downloads: 18208
aircraft wing spar computational technique Finite Element Analysis (FEA) graphite-epoxy design shear force and bending moment
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Graphite-Epoxy Composite Design for Aircraft Wing Skin Using Computational Techniques - Part II
by Akindapo Jacob Olaitan and Johnson-Anamemena Nnaemeka, Garba Danladi King
American Journal of Mechanical Engineering. 2017, 5(5), 175-198. DOI: 10.12691/ajme-5-5-1
Pub. Date: September 25, 2017Views: 17510Downloads: 13718
aircraft wing skin epoxy graphite high modulus low modulus ultra modulus
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