Email this article Reliability Providing Approach for Structurally- Parametrical Optimization Results of an “Aggressive” Intermediate Duct of the Bypass Gas-Turbine Engine
- Authors: Vinogradov K.A.1, Remizov A.E.2, Vinogradova O.V.1
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Affiliations:
- NPO Saturn
- Soloviev Rybinsk State Aviation Technical University
- Issue: Vol 61, No 3 (2018)
- Pages: 384-390
- Section: Aero- and Gas-Dynamics of Flight Vehicles and Their Engines
- URL: https://journals.rcsi.science/1068-7998/article/view/230599
- DOI: https://doi.org/10.3103/S1068799818030108
- ID: 230599
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Abstract
Limit assessment for the new optimization approach is carried out. This approach allows us to optimize the gas turbine duct elements by using the structural analysis and computational fluid dynamics methods, and to minimize the necessary number of CFD computations. Obtained results were verified and confirmed by experimental aerodynamic investigation.
About the authors
K. A. Vinogradov
NPO Saturn
Author for correspondence.
Email: keryisdex@mail.ru
Russian Federation, pr. Lenina 163, Rybinsk, Yaroslavskaya oblast, 152903
A. E. Remizov
Soloviev Rybinsk State Aviation Technical University
Email: keryisdex@mail.ru
Russian Federation, ul. Pushkina 53, Rybinsk, Yaroslavskaya oblast, 152934
O. V. Vinogradova
NPO Saturn
Email: keryisdex@mail.ru
Russian Federation, pr. Lenina 163, Rybinsk, Yaroslavskaya oblast, 152903
