Email this article Composite gas-turbine blades
- Authors: Eliseev V.V.1, Piskunov V.A.1
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Affiliations:
- Peter the Great Saint Petersburg Polytechnic University
- Issue: Vol 36, No 10 (2016)
- Pages: 819-822
- Section: Article
- URL: https://journals.rcsi.science/1068-798X/article/view/227048
- DOI: https://doi.org/10.3103/S1068798X16100087
- ID: 227048
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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.
About the authors
V. V. Eliseev
Peter the Great Saint Petersburg Polytechnic University
Author for correspondence.
Email: yeliseyev@inbox.ru
Russian Federation, St. Petersburg
V. A. Piskunov
Peter the Great Saint Petersburg Polytechnic University
Email: yeliseyev@inbox.ru
Russian Federation, St. Petersburg
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