| タイトル | Compressor Flow Control Concepts |
| 著者（英） | Chima, Rodrick V. |
| 著者所属（英） | NASA Glenn Research Center |
| 発行日 | 2001-01-01 |
| 言語 | eng |
| 内容記述 | Several passive flow control devices have been modeled computationally in the Swift CFD code. The models were applied to the first stage rotor and stator of the baseline UEET compressor in an attempt to improve efficiency and/or stall margin. The devices included suction surface bleed, tip injection, self-aspirated rotors, area-ruled casing, and vortex generators. The models and computed results will be described in the presentation. None of the results have shown significant gains in efficiency; however, casing vortex generators have shown potential improvements in stall margin. |
| NASA分類 | Aircraft Propulsion and Power |
| 権利 | No Copyright |
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