| タイトル | Measurement of the Coolant Channel Temperatures and Pressures of a Cooled Radial-Inflow Turbine |
| 本文（外部サイト） | http://hdl.handle.net/2060/19940029200 |
| 著者（英） | Dicicco, L. Danielle; Tirres, Lizet; Nowlin, Brent C. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1994-06-01 |
| 言語 | eng |
| 内容記述 | Instrumentation has been installed on the surface of a cooled radial-inflow turbine. Thermocouples and miniature integrated sensor pressure transducers were installed to measure steady state coolant temperatures, blade wall temperatures, and coolant pressures. These measurements will eventually be used to determine the heat transfer characteristics of the rotor. This paper will describe the procedures used to install and calibrate the instrumentation and the testing methods followed. A limited amount of data will compare the measured values to the predicted values. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 94N33706
AIAA PAPER 94-2561 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
