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Combination probes for stagnation pressure and temperature measurements in gas turbine engines

机译：燃气轮机发动机停滞压力和温度测量的组合探头

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C Bonham; S J Thorpe; M N Erlund; R J Stevenson;
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1. High-temperature high-frequency turbine exit flow field measurements in a military engine with a cooled unsteady total pressure probe [J] . M Mersinligil, J Desset, J F Brouckaert Proceedings of the Institution of Mechanical Engineers . 2011,第7期

机译：带冷却的非稳态总压力探头的军用发动机中的高温高频涡轮机出口流场测量
2. High-temperature high-frequency turbine exit flow field measurements in a military engine with a cooled unsteady total pressure probe [J] . Journal of Power and Energy . 2011,第7期

机译：带冷却的非稳态总压力探头的军用发动机中的高温高频涡轮机出口流场测量
3. High-temperature high-frequency turbine exit flow field measurements in a military engine with a cooled unsteady total pressure probe [J] . M Mersinligil, J Desset, J F Brouckaert Proceedings of the Institution of Mechanical Engineers . 2011,第A7期

机译：带冷却的非稳态总压力探头的军用发动机中的高温高频涡轮机出口流场测量
4. FIRST UNSTEADY PRESSURE MEASUREMENTS WITH A FAST RESPONSE COOLED TOTAL PRESSURE PROBE IN HIGH TEMPERATURE GAS TURBINE ENVIRONMENTS [C] . Mehmet MERSINLIGIL, Jean-Frangois BROUCKAERT, Julien DESSET ASME turbo expo . 2011

机译：高温燃气轮机环境中具有快速响应冷却总压力探头的首次非稳态压力测量
5. Coherent anti-Stokes Raman scattering for quantitative temperature and concentration measurements in a high-pressure gas turbine combustor rig. [D] . Thariyan, Mathew Paul. 2010

机译：相干的反斯托克斯拉曼散射，用于在高压燃气轮机燃烧器装置中进行定量温度和浓度测量。
6. High-Pressure Geoscience Special Feature: Indoor seismology by probing the Earths interior by using sound velocity measurements at high pressures and temperatures [O] . Baosheng Li, Robert C. Liebermann 2007

机译：高压地球科学专题：通过在高压和高温下使用声速测量来探测地球内部从而进行室内地震
7. Development of a small-sized acoustic probe for the measurement of pressure pulsations in the gasdynamic duct of gas turbine engines [O] . A. G. Gimadiyev, N. D. Bystrov, S. A. Ilyinsky 2014

机译：用于测量燃气涡轮发动机汽油管道压力脉动的小型声学探头的开发

Combination probes for stagnation pressure and temperature measurements in gas turbine engines

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