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Strength design model for thin-walled structures

  • Technical Notes/Structural Mechanics and Strength of Flight Vehicles
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Abstract

In this paper, the finite element analysis of the stress-strain state for cylindrical structures is discussed. In this case, various fundamental hypotheses can be used in the framework of a model that is of interest for design and optimization. Numerical examples are presented to evaluate the possibilities of this model.

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References

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Authors and Affiliations

  1. Nanjing University of Aeronautics and Astronautics, 29 Yudao St., Nanjing, 210016, China

    Z. J. Wang, L. H. Kang & S. Huang

  2. Tupolev Kazan National Research Technical University, ul. Karla Marksa 10, Kazan, 420111, Tatarstan, Russia

    A. S. Kretov

Authors
  1. Z. J. Wang
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  2. L. H. Kang
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  3. A. S. Kretov
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  4. S. Huang
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Corresponding author

Correspondence to Z. J. Wang.

Additional information

Original Russian Text © Z.J. Wang, L.H. Kang, A.S. Kretov, H. Sheng, 2016, published in Izvestiya VUZ, Aviatsionnaya Tekhnika, 2016, No. 1, pp. 116–122.

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Wang, Z.J., Kang, L.H., Kretov, A.S. et al. Strength design model for thin-walled structures. Russ. Aeronaut. 59, 126–133 (2016). https://doi.org/10.3103/S1068799816010207

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  • DOI: https://doi.org/10.3103/S1068799816010207

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