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Composite gas-turbine blades

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Abstract

Theoretical analysis of composite blades for gas-turbine engines is based on the theory of effective moduli and the Lagrange equations. The blades are regarded as twisted rods; the flexure-approximation coefficients are adopted as generalized coordinates.

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Authors and Affiliations

  1. Peter the Great Saint Petersburg Polytechnic University, St. Petersburg, Russia

    V. V. Eliseev & V. A. Piskunov

Authors
  1. V. V. Eliseev
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  2. V. A. Piskunov
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Corresponding author

Correspondence to V. V. Eliseev.

Additional information

Original Russian Text © V.V. Eliseev, V.A. Piskunov, 2016, published in Vestnik Mashinostroeniya, 2016, No. 7, pp. 42–44.

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Eliseev, V.V., Piskunov, V.A. Composite gas-turbine blades. Russ. Engin. Res. 36, 819–822 (2016). https://doi.org/10.3103/S1068798X16100087

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  • DOI: https://doi.org/10.3103/S1068798X16100087

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