| タイトル | Modeling of Broadband Liners Applied to the Advanced Noise Control Fan |
| 本文（外部サイト） | http://hdl.handle.net/2060/20160006058 |
| 著者（英） | Sutliff, Daniel L.; Nark, Douglas M.; Jones, Michael G. |
| 発行日 | 2015-06-22 |
| 言語 | eng |
| 内容記述 | The broadband component of fan noise has grown in relevance with an increase in bypass ratio and incorporation of advanced fan designs. Therefore, while the attenuation of fan tones remains a major factor in engine nacelle acoustic liner design, the simultaneous reduction of broadband fan noise levels has received increased interest. As such, a previous investigation focused on improvements to an established broadband acoustic liner optimization process using the Advanced Noise Control Fan (ANCF) rig as a demonstrator. Constant-depth, double-degree of freedom and variable-depth, multi-degree of freedom liner designs were carried through design, fabrication, and testing. This paper addresses a number of areas for further research identified in the initial assessment of the ANCF study. Specifically, incident source specification and uncertainty in some aspects of the predicted liner impedances are addressed. This information is incorporated in updated predictions of the liner performance and comparisons with measurement are greatly improved. Results illustrate the value of the design process in concurrently evaluating the relative costs/benefits of various liner designs. This study also provides further confidence in the integrated use of duct acoustic propagation/radiation and liner modeling tools in the design and evaluation of novel broadband liner concepts for complex engine configurations. |
| NASA分類 | Acoustics; Aircraft Propulsion and Power |
| レポートNO | NF1676L-20210 |
| 権利 | No Copyright |
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