Research on Nonlinear Deformation and Stability of an Advanced Aircraft Fuselage Composite Section under Pure Bending |
| |
| Authors: | V K Belov L P Zheleznov T S Ognyanova |
| |
| Institution: | 1.S. A. Chaplygin Aeronautical Research Institute (SibNIA),Novosibirsk,Russia |
| |
| Abstract: | The finite element algorithm developed by the authors has been used for solving the strength and stability problems of shells. The effect of deformation nonlinearity, stiffness of stringer set, shell thickness on critical loads has been determined. |
| |
| Keywords: | |
| 本文献已被 SpringerLink 等数据库收录！ |
