| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 8059125 | Propulsion and Power Research | 2018 | 13 Pages |
Abstract
The aerodynamic performances of the generated tandem-blade cascades are obtained using two-dimensional numerical solution of flow. For this, a viscous turbulent flow solver is used for solving the Navier-Stokes equations. In these simulations, inlet Mach number is fixed to 0.6.
Related Topics
Physical Sciences and Engineering
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Energy Engineering and Power Technology
Authors
Behshad Ghazanfari, Mahdi Nili-Ahmadabadi, Ashkan Torabi-Farsani, Mohammad Hossein Noorsalehi,