| タイトル | Langley 8-foot high-temperature tunnel oxygen measurement system |
| 著者（英） | Chen, Tony D.; Chaturvedi, Sushil K.; Sprinkle, Danny R. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1991-05-01 |
| 言語 | eng |
| 内容記述 | In order to ensure that there is a proper amount of oxygen necessary for sustaining test engine operation for hypersonic propulsion systems testing at the NASA Langley 8-foot high-temperature tunnel, a quickly responding real-time measurement system of test section oxygen concentration has been designed and tested at Langley. It is built around a zirconium oxide-based sensor which develops a voltage proportional to the oxygen partial pressure of the test gas. The voltage signal is used to control the amount of oxygen being injected into the combustor air. The physical operation of the oxygen sensor is described, as well as the sampling system used to extract the test gas from the tunnel test section. Results of laboratory tests conducted to verify sensor accuracy and response time performance are discussed, as well as the final configuration of the system to be installed in the tunnel. |
| NASA分類 | RESEARCH AND SUPPORT FACILITIES (AIR) |
| レポートNO | 93A44892 |
| 権利 | Copyright |
|
