| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 10281949 | Applied Energy | 2012 | 13 Pages |
Abstract
⺠The 2D and 3D CIRCLE method is presented and used to design high-efficiency turbomachinery blades and isolated airfoils. ⺠Two 2D turbine blades, one compressor blade, and one isolated airfoil geometry are redesigned. ⺠The aerodynamic advantages of the redesigned blades are investigated. ⺠A 3D compressor and a 3D turbine blade are designed with the method and their aerodynamic performance is computed. ⺠It is concluded the method is a robust tool for the design of high-efficiency 2D and 3D blades and airfoils.
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Authors
T. Korakianitis, I.A. Hamakhan, M.A. Rezaienia, A.P.S. Wheeler, E.J. Avital, J.J.R. Williams,