| タイトル | Acoustic emission studies of large advanced composite rocket motor cases. |
| 著者（英） | Robinson, E. Y. |
| 発行日 | 1973-01-01 |
| 言語 | eng |
| 内容記述 | Acoustic emission (AE) patterns were measured during pressure testing of advanced composite rocket motor cases made of boron/epoxy and graphite/epoxy. Both accelerometers and high frequency AE transducers were used, and both frequency spectrum and amplitude distribution were studied. The AE patterns suggest that precursor emission might be used in certain cases to anticipate failure. The technique of hold-cycle AE monitoring was also evaluated and could become a valuable decision gate for test continuation/termination. Data presented show similarity of accelerometers and AE transducer responses despite the different frequency response, and suggest that structural AE phenomena are broadband. |
| NASA分類 | STRUCTURAL MECHANICS |
| レポートNO | 73A23967 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/458094 |
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