Enviar artigo por via de e-mail Composite gas-turbine blades
- Autores: Eliseev V.V.1, Piskunov V.A.1
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Afiliações:
- Peter the Great Saint Petersburg Polytechnic University
- Edição: Volume 36, Nº 10 (2016)
- Páginas: 819-822
- Seção: Article
- URL: https://journal-vniispk.ru/1068-798X/article/view/227048
- DOI: https://doi.org/10.3103/S1068798X16100087
- ID: 227048
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Resumo
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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Sobre autores
V. Eliseev
Peter the Great Saint Petersburg Polytechnic University
Autor responsável pela correspondência
Email: yeliseyev@inbox.ru
Rússia, St. Petersburg
V. Piskunov
Peter the Great Saint Petersburg Polytechnic University
Email: yeliseyev@inbox.ru
Rússia, St. Petersburg
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