English
The effects of simulated lightning strikes and currents on aircraft bonded joints and access/inspection panels were investigated. Both metallic and composite specimens were tested. Tests on metal fuel feed through elbows in graphite/epoxy structures were evaluated. Sparking threshold and residual strength of single lap bonded joints and sparking threshold of access/inspection panels and metal fuel feed through elbows are reported.
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CRYSTAL GROWTH · PRECIPITATES · SCANNING ELECTRON MICROSCOPY · SOLAR COLLECTORS · CRYSTAL STRUCTURE · FLAT PLATES · GRAIN BOUNDARIES · SEMICONDUCTORS (MATERIALS) · SILICON · CARRIER LIFETIME