Finite Element Analysis of Composite Shell Structure of Aircraft Wing Using Composite Structure

The simplified methods of the wing structures can be performed with enough confidence; as long as the simplified method based designs are analysts. The analysis result shows that the simplified method is applicable to used for performing the wing structure. During the analysis depending on the meshing is used from software package as MSC/PATRAN. Conclusions are also inferred with regard to the deficiency of certain element types in handling the true external load and internal load acting on the wing structure.