Nonlinear deforming of laminated composite shells of revolution under finite deflections and normal’s rotation angles
Russian aeronautics ; 60 , 2
2017
Article (Journal)
English
BKL: | 55.50 Luftfahrzeugtechnik | |
Local classification TIB: | 770/7040/8000 |
Calculation of finite axisymmetric deflections of thin short shells of revolution
British Library Online Contents | 1996
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