摘要
本文详细介绍了高频响温度传感器的设计、校准、误差分析及修正技术,并结合发动机进气温度畸变试验研究了高频响温度测试技术和数据处理方法,对航空发动机稳定性评定试验研究具有重要的指导意义。
This paper has detailed the design, calibration and error analysis of a high frequency response temperature probe. It also studies the high frequency response temperature measurement and data processing in aero-engine inlet temperature distortion test. This is of great importance to aero-engine stability assessment test.
出处
《燃气涡轮试验与研究》
2005年第2期41-48,共8页
Gas Turbine Experiment and Research
