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Analysis of shells of revolution under symmetrical loading using the quadrature method

  • Structural Mechanics and Strength of Flight Vehicles
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Abstract

The application of the quadrature method [1] to analyzing the shells of revolution under symmetrical loading relative to the zero meridian is considered. The method can be treated as a generalization of the method presented in [2] to solve the Volterra integral equation of the second kind.

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References

  1. Akhmed’yanov, I.S., Application of the Quadrature Method to Integration of the Decisive System of Differential Equations for Shells of Revolution Bending, Izv. AN SSSR. Mekhanika Tverdogo Tela, 1990, no. 4, pp. 83–87.

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Authors and Affiliations

  1. Samara State Aerospace University, Samara, Russia

    I. S. Akhmed’yanov

Authors
  1. I. S. Akhmed’yanov
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Additional information

Original Russian Text © I.S. Akhmed’yanov, 2009, published in Izvestiya VUZ. Aviatsionnaya Tekhnika, 2009, No. 4, pp. 8–11.

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Akhmed’yanov, I.S. Analysis of shells of revolution under symmetrical loading using the quadrature method. Russ. Aeronaut. 52, 383–389 (2009). https://doi.org/10.3103/S1068799809040023

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  • DOI: https://doi.org/10.3103/S1068799809040023

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