508: A320 Sharklets

Linear static stress and linear buckling analysis of a support structure for a A320 winglet. Multiple load cases were analysed, subjecting the design to a number of different support locations whilst supporting the dead weight of the frame and winglet. For all load cases, the minimum factor of safety on yield strength and minimum buckling load multiplier was acceptable.

508 - FEA-Solutions (UK) Ltd - Finite Element Analysis For Your Product Design

508: A320 Sharklets

Linear static stress and linear buckling analysis of a support structure for a A320 winglet. Multiple load cases were analysed, subjecting the design to a number of different support locations whilst supporting the dead weight of the frame and winglet. For all load cases, the minimum factor of safety on yield strength and minimum buckling load multiplier was acceptable.