Numerical analysis with experimental data of the joint of fuselage with main landing gear and wing‐strut, of a two‐seat aircraft built with composites

Publisher： John Wiley & Sons Inc

E-ISSN： 1548-0569|36|6|1072-1083

ISSN： 0272-8397

Source： POLYMER COMPOSITES, Vol.36, Iss.6, 2015-06, pp. : 1072-1083

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