A Simple Way for the Detail Component Design of Aircraft Wings

摘要

Due to the lack of the wings detail design progress and the limitation of ordinary detail design ways for the complicated design of wings, while a new wing detail design process was proposed based on traditional wing structural design approach. The process involves taking loads on initial proofing structure, structural design, FEM (Finite Element Methods) analysis, etc. According to the wing structural characteristics, it makes the reaction forces as the input loads for the detail design. The detail components are designed based on the new design process which meets to all the design requirements. It shows that the new design process is feasible and available.