| タイトル | Parametric Testing of Chevrons on Single Flow Hot Jets |
| 本文（外部サイト） | http://hdl.handle.net/2060/20040152072 |
| 著者（英） | Brown, Clifford A.; Bridges, James |
| 著者所属（英） | NASA Glenn Research Center |
| 発行日 | 2004-09-01 |
| 言語 | eng |
| 内容記述 | A parametric family of chevron nozzles have been studied, looking for relationships between chevron geometric parameters, flow characteristics, and far-field noise. Both cold and hot conditions have been run at acoustic Mach number 0.9. Ten models have been tested, varying chevron count, penetration, length, and chevron symmetry. Four comparative studies were defined from these datasets which show: that chevron length is not a major impact on either flow or sound; that chevron penetration increases noise at high frequency and lowers it at low frequency, especially for low chevron counts; that chevron count is a strong player with good low frequency reductions being achieved with high chevron count without strong high frequency penalty; and that chevron asymmetry slightly reduces the impact of the chevron. Finally, it is shown that although the hot jets differ systematically from the cold one, the overall trends with chevron parameters is the same. |
| NASA分類 | Aircraft Propulsion and Power |
| レポートNO | NASA/TM-2004-213107
AIAA Paper 2004-2824
E-14582 |
| 権利 | No Copyright |
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