Tharan Gordon
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Two-stage gust load alleviating torsional stiffness device for hinged aircraft wingtips Open
This article introduces a novel mechanism exhibiting a two-stage, non-linear softening torsional stiffness designed to improve the aerodynamic performance of the Semi-Aeroelastic Hinged wingtip concept, while retaining its gust load allevi…
Suppression of compression induced delamination in tapered laminated composites using a ply scarfing method Open
Thickness tapering of composite laminates is a common strategy for efficient and lightweight composite structures. The termination of specific plies necessary to achieve such tapering is well known to introduce sites for delamination initi…