| タイトル | Generation of desired signals from acoustic drivers |
| 著者（英） | Ahuja, K. K.; Ramakrishnan, R.; Salikuddin, M. |
| 著者所属（英） | Lockheed-Georgia Co. |
| 発行日 | 1982-11-08 |
| 言語 | eng |
| 内容記述 | A procedure to control transient signal generation is developed for the study of internal noise propagation from aircraft engines. A simple algorithm incorporating transform techniques is used to produce signals of any desired waveform from acoustic drivers. The accurate driver response is then calculated, and from this the limiting frequency characteristics are determined and the undesirable frequencies where the driver response is poor are eliminated from the analysis. A synthesized signal is then produced by convolving the inverse of the response function with the desired signal. Although the shape of the synthesized signal is in general quite awkward, the driver generates the desired signal when the distorted signal is fed into the driver. The results of operating the driver in two environments, in a free field and in a duct, are presented in order to show the impedance matching effect of the driver. In addition, results using a high frequency cut-off value as a parameter is presented in order to demonstrate the extent of the applicability of the synthesis procedure. It is concluded that the desired signals can be generated through the signal synthesis procedure. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 83A15068 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/406449 |
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