This document constitutes the final report on the structural analysis and design of boron-epoxy wing skins. The design and fabrication of boron composite laminate skins are intended to replace the upper and lower structural covers of the F-100D wing. This report presents the final design of these boron-epoxy wing skins and the material properties and structural analysis. Structural optimization and analysis are presented. (P.S.-PL)
Boron-Epoxy Wing Skins F-100D Aircraft Structural Design and Analysis
1971
114 pages
Report
No indication
English
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