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Dependence of helicopter lifting system loading on temperature variations in composite material properties

  • Structural Mechanics and Strength of Flight Vehicles
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Abstract

The results of studying the influence of physical and mechanical properties of composite materials on balancing characteristics and loading of a helicopter under changes of climatic operational conditions are described.

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References

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Authors and Affiliations

  1. Tupolev State Technical University, Kazan, Russia

    S. A. Mikhailov, A. M. Girfanov & A. B. Bochkareva

  2. OAO Kazan Helicopters, Kazan, Russia

    A. S. Fal’ko

Authors
  1. S. A. Mikhailov
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  2. A. M. Girfanov
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  3. A. B. Bochkareva
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  4. A. S. Fal’ko
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Additional information

Original Russian Text © S.A. Mikhailov, A.M. Girfanov, A.B. Bochkareva, A.S. Fal’ko, 2008, published in Izvestiya VUZ. Aviatsionnaya Tekhnika, 2008, No. 1, pp. 13–16.

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Mikhailov, S.A., Girfanov, A.M., Bochkareva, A.B. et al. Dependence of helicopter lifting system loading on temperature variations in composite material properties. Russ. Aeronaut. 51, 11–15 (2008). https://doi.org/10.3103/S1068799808010030

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  • DOI: https://doi.org/10.3103/S1068799808010030

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