Stability analysis on the ribbed panel of the composite wing

作者：Huo S^*; Wang F; Wang P; Yue Z

来源：Chinese Journal of Applied Mechanics, 2010, 27(2): 423-427.

• Boundary conditions
• Composite materials
• Ribbed panel
• Stability
• Stringer

The overall and local buckling of the ribbed panel is analyzed by project and finite element methods in this paper. The study shows that the choice of boundary conditions in the finite element method has a great influence on the results. The stability of the ribbed panel in different boundary conditions is analyzed by using the FE software of MSC. Patran. Compared the results with the project method, an appropriate choice of the model and boundary conditions is put forward. The stability of the ribbed panel with the same area of the stringer and different stringer designs is analyzed by using the model and boundary conditions mentioned above. The results show that the design of the stringer cross section has a great influence on the stability of the ribbed panel.

• 出版日期2010
• 单位西北工业大学