Figure 6. MATLAB generated plot for the various load components along the length of the aircraft wing

From

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

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

American Journal of Mechanical Engineering. 2017, 5(4), 117-127 doi:10.12691/ajme-5-4-2