Numerical Investigation on Metrological Fidelity of a Shielded Thermocouple Probe and the Effects of Geometrical Parameters

Author:

Ummer Zahir12,Zhang Weihao12,Yang Weiping1,Zou Zhengping12,Zhao Jian3

Affiliation:

1. National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, School of Energy and Power Engineering , Beihang University , Beijing 100191 , China

2. Collaborative Innovation Center of Advanced Aero-Engine , Beijing 100191 , China

3. Beijing Changcheng Institute of Metrology and Measurement, Science and Technology on Metrology and Calibration Laboratory , Beijing 100095 , China

Abstract

Abstract Proper design optimization and precise error characterization of temperature sensing-elements are rudimentary in the field of high accuracy gas temperature measurements. The intricate flow structures and heat transfer mechanisms related to a shielded thermocouple probe are studied in this paper using computational fluid dynamics and conjugate heat transfer (CFD/CHT) simulation tools. Owing to the probe’s novel geometry, it was a pre-requisite to characterize the metrological fidelity of the probe and the steady-state errors were determined from the simulations. The influence of certain geometrical parameters on the error characteristics of the probe was also investigated. The characteristic variation of the metrological fidelity of the probe with respect to those geometrical parameters should facilitate the optimization of the probe design.

Publisher

Walter de Gruyter GmbH

Subject

Aerospace Engineering

Reference28 articles.

1. Fiock EF, Dahl AI. Shielded thermocouples for gas turbines. Trans ASME. 1949;71:147–53.

2. Hill P, Peterson C. Mechanics and thermodynamics of propulsion, 2nd ed. New Jersey, US: Prentice Hall, 1991.

3. Bonham C, Thorpe SJ, Erlund MN, Stevenson RD. Stagnation temperature measurement using thin-film platinum resistance sensors. Meas Sci Technol. 2014;25:1–16.

4. Saravanamuttoo HI. Recommended practices for measurement of gas path pressures and temperatures for performance assessment of aircraft turbine engines and components. Report No. 245. AGARD Advisory, 1990.

5. Winkler E. Design and calibration of stagnation temperature probes for use at high supersonic speeds and elevated temperatures. J Appl Phys. 1954;25:231–2.

Cited by 5 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3