Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Tai-qiu Liu"'
Publikováno v:
Energies, Vol 9, Iss 4, p 296 (2016)
This paper describes the introduction of three-dimension (3-D) blade designs into a 5-stage axial compressor with multi-stage computational fluid dynamic (CFD) methods. Prior to a redesign, a validation study is conducted for the overall performance
Externí odkaz:
https://doaj.org/article/dae3701db6a1432d9f43ca7548d32658
Publikováno v:
Aerospace Science and Technology. 52:81-94
Resume This paper outlines the aerodynamic optimization of stator vane settings for multi-stage compressors via the combination of an artificial neural network (ANN) and a genetic algorithm (GA). The investigation is conducted on a newly developed 5-
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f3d116c7596a2a22b24686a8c8598581
https://doi.org/10.1016/j.ast.2016.02.024
https://doi.org/10.1016/j.ast.2016.02.024
Publikováno v:
Science China Technological Sciences. 59:93-108
In this paper, a novel engineering platform for throughflow analysis based on streamline curvature approach is developed for the research of a 5-stage compressor. The method includes several types of improved loss and deviation angle models, which ar
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::070c84301853e081a1421c82d3716c0c
https://doi.org/10.1007/s11431-015-5947-4
https://doi.org/10.1007/s11431-015-5947-4
Publikováno v:
Volume 2C: Turbomachinery.
An optimization method combined of a genetic algorithm, an artificial neural network, a CFD solver and a blade generator, is developed in this research and applied in the three-dimensional blading design of a newly designed highly-loaded 5-stage axia
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b36181bea925bb6ffdc48b7a820e30fd
https://doi.org/10.1115/gt2016-57626
https://doi.org/10.1115/gt2016-57626
Publikováno v:
Volume 2A: Turbomachinery.
The paper is a preliminary methodology research of the aerodynamic redesign of a 5-stage axial compressor by re-stagger and bow with multistage CFD methods, with the purpose of developing the next upgrade version of this type of compressor. Prior to
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::75db92e13a054938c2d14fbde5807772
https://doi.org/10.1115/gt2015-42877
https://doi.org/10.1115/gt2015-42877
Development of a Throughflow Method for Aerodynamic Analysis of Highly Loaded Axial Flow Compressors
Publikováno v:
Volume 2B: Turbomachinery.
In this paper, a novel engineering platform for throughflow analysis based on streamline curvature approach is developed for the research of a 5-stage compressor. It includes several types of improved loss and deviation angle models for the purpose o
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6e5c86574e7349ac0c3a8250b29e789d
https://doi.org/10.1115/gt2015-42020
https://doi.org/10.1115/gt2015-42020