Analysis of flight vehicle stiffened section skin stability in shear |
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| Authors: | O V Borisova |
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| Institution: | 1.Samara State Aerospace University,Samara,Russia |
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| Abstract: | The skin panels of riveted cylindrical sections of flight vehicles in shear are considered. The objective of the analysis
based on the finite element method is to verify the recommendations available for determining critical stresses of similar
structural elements and to obtain new results for practical calculations. |
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