ePrints Soton (University of Southampton) · 2016 · 11 citations · 0 references
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EngineeringAerospace EngineeringMechanical EngineeringAerodynamicsAeroelasticityAircraft DesignAeroelastic LoadsAeroelastic ModelingAeroelastic Response PredictionAeroelastic StabilityDynamic AeroelasticityWing DesignAeroelastic EffectsAeroelastic ResponseHigh-aspect-ratio Wing AeroelasticityWing AeroelasticityWing Flutter AnalysisWing Tip StructuresWing Weight Reduction
The primary purpose of a hinged wing tip on an airliner aircraft is to allow an aerodynamically efficient high aspect ratio wing to enter an airport gate of standard dimensions. There exists a potential opportunity to allow a wing tip to move in flight to alleviate the loads and achieve a lower wing weight. This paper will provide a summary of the latest studies investigating the Aeroelastic behaviour (loads and flutter) of hinged wing tips.