Optimization approach and some results for 2D compressor airfoil / Komarov O.V., Sedunin V.A., Blinov V.L., Serkov S.A. // International Journal of Gas Turbine, Propulsion and Power Systems. - 2016. - V. 8, l. 3. - P. 39-46.

ISSN:
18825079
Type:
Article
Abstract:
Several optimization approaches are presented in the paper, and the results of each task depending on the optimization setup are compared and discussed in terms of physical behavior and convergence. The optimization problem is set up and solved for several 2D compressor airfoils with different inlet parameters. The airfoils were generated and their characteristics were built for optimized solutions from different optimization approaches. The novel topology for 2D compressor airfoil is proposed and successfully utilized. The approach was tested for particular cases and showed a gain in efficiency and flow turning up to 15% (relative) compared with NACA-65 airfoils taken as the initial design. Copyright © 2016 Gas Turbine Society of Japan.
Author keywords:
Index keywords:
Compressors; Optimization; Compressor airfoils; Flow turning; Initial design; Optimization approach; Optimization problems; Optimized solutions; Physical behaviors; Airfoils
DOI:
нет данных
Смотреть в Scopus:
https://www.scopus.com/inward/record.uri?eid=2-s2.0-85007294087&partnerID=40&md5=2c2ec55cae88b33a00e6baa3aff0c434
Соавторы в МНС:
Другие поля
Поле Значение
Link https://www.scopus.com/inward/record.uri?eid=2-s2.0-85007294087&partnerID=40&md5=2c2ec55cae88b33a00e6baa3aff0c434
Affiliations Ural Federal University, Turbines and Engines Department, Yekaterinburg, Russian Federation
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Publisher Gas Turbine Society of Japan
Language of Original Document English
Abbreviated Source Title Int. J. Gas Turbine Propul. Power Syst.
Source Scopus