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Modeling and analysis of composite hinge for aircraft spoiler using finite element analysis.

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Figure 1.1 : Rolling Motion Cause by Deploying Right Spoiler (NASA, 2010)
Figure 1.2 : FACC Carbon Composite Center Hinge Fitting (Dawson, 2006): (a) Metal  Bushings and Bearings Installed in the Fitting Lugs; (b) Hinge Fitting Molded via RTM
Figure 1.3 : Composite Structural Weight Development in Airbus (Bold, 2007)

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