Boron-Epoxy Wing Skins F-100D Aircraft Structural Design and Analysis.

摘要

The design and fabrication of boron composite laminate skins to replace the upper and lower structural covers of the F- 100D wing accepts all the functional design requirements, constraints, and structural loads of the original design. The design of boron-epoxy wing skins, the material properties and structural analysis are presented. The procedures used for selecting the laminate orientation and stiffened panel configurations are discussed. (P.S.-PL)