| タイトル | Thin film temperature sensors, phase 3 |
| 本文（外部サイト） | http://hdl.handle.net/2060/19820014605 |
| 著者（英） | Grant, H. P.; Claing, R. G.; Przybyszewski, J. S.; Anderson, W. L. |
| 著者所属（英） | Pratt and Whitney Aircraft Group |
| 発行日 | 1982-01-11 |
| 言語 | eng |
| 内容記述 | A thin film thermocouple system installation suitable for engine test evaluation was designed, and an engine test plan was prepared. Film adherence, durability, accuracy, and drift characteristics were improved. Film thickness was increased to 14 microns, and drift was reduced to less than 0.02 percent of Fahrenheit temperature per hour on actual turbine blades at 1255 K. |
| NASA分類 | INSTRUMENTATION AND PHOTOGRAPHY |
| レポートNO | 82N22479
PWA-5708-26
NAS 1.26:165476
NASA-CR-165476 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/166301 |
