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Modeling the Transformation of Hexactinal Folded Structure

  • Aircraft and Rocket Engine Design and Development
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Abstract

A mathematical model is developed to study the transformation of hexactinal folded structures. Equations for calculation of the structure element pathways during transformation are obtained based on the vector analysis methods. An algorithm is presented together with a model problem solution.

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Acknowledgements

The work is supported by the Ministry of Science and Higher Education, the project unique identification number is RFMEFI57717X0262.

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Authors and Affiliations

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

    A. V. Shabalov, V. I. Khaliulin & N. V. Levshonkov

  2. Kazan State Power Engineering University, ul. Krasnosel’skaya 51, Kazan, Tatarstan, 420066, Russia

    R. Sh. Gimadiev

Authors
  1. A. V. Shabalov
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  2. V. I. Khaliulin
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  3. R. Sh. Gimadiev
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  4. N. V. Levshonkov
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Corresponding author

Correspondence to V. I. Khaliulin.

Additional information

Russian Text © The Author(s), 2019, published in Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2019, No. 2, pp. 108–117.

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Shabalov, A.V., Khaliulin, V.I., Gimadiev, R.S. et al. Modeling the Transformation of Hexactinal Folded Structure. Russ. Aeronaut. 62, 287–297 (2019). https://doi.org/10.3103/S1068799819020168

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  • DOI: https://doi.org/10.3103/S1068799819020168

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