| タイトル | The Effect of Pulse Length and Ejector Radius on Unsteady Ejector Performance |
| 本文（外部サイト） | http://hdl.handle.net/2060/20050214754 |
| 著者（英） | Wilson, Jack |
| 著者所属（英） | QSS Group, Inc. |
| 発行日 | 2005-08-01 |
| 言語 | eng |
| 内容記述 | The thrust augmentation of a set of ejectors driven by a shrouded Hartmann-Sprenger tube has been measured at four different frequencies. Each frequency corresponded to a different length to diameter ratio of the pulse of air leaving the driver shroud. Two of the frequencies had length to diameter ratios below the formation number, and two above. The formation number is the value of length to diameter ratio below which the pulse converts to a vortex ring only, and above which the pulse becomes a vortex ring plus a trailing jet. A three level, three parameter Box-Behnken statistical design of experiment scheme was performed at each frequency, measuring the thrust augmentation generated by the appropriate ejectors from the set. The three parameters were ejector length, radius, and inlet radius. The results showed that there is an optimum ejector radius and length at each frequency. Using a polynomial fit to the data, the results were interpolated to different ejector radii and pulse length to diameter ratios. This showed that a peak in thrust augmentation occurs when the pulse length to diameter ratio equals the formation number, and that the optimum ejector radius is 0.87 times the sum of the vortex ring radius and the core radius. |
| NASA分類 | Aircraft Propulsion and Power |
| レポートNO | NASA/CR-2005-213796
E-15154
AIAA Paper 2005-3829 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/219443 |
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