| タイトル | High temperature strain gage technology for hypersonic aircraft development applications |
| 本文（外部サイト） | http://hdl.handle.net/2060/19920012996 |
| 著者（英） | Anderson, W. L.; Grant, H. P. |
| 著者所属（英） | Pratt and Whitney Aircraft |
| 発行日 | 1992-02-01 |
| 言語 | eng |
| 内容記述 | An experimental evaluation of Pd 13 percent Cr and of BCL-3 alloy wire strain gages was conducted on IN100 and Cu 0.15 percent Zr alloy substrates. Testing included apparent strain, drift, gage factor, and creep. Maximum test temperature was 1144 K (1600 F). The PdCr gages incorporated Pt temperature compensation elements. The PdCr gages were found to have good resistance stability below 866 K (1100 F). The BCL 3 gages were found to have good resistance stability above 800 K (981 F), but high drift around 700 K (800 F). |
| NASA分類 | INSTRUMENTATION AND PHOTOGRAPHY |
| レポートNO | 92N22239
PWA-6141
NAS 1.26:189101
NASA-CR-189101 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/127945 |
