Optimal design of steady enthalpy probe and test verification

ZHU Xinxin; LONG Yongsheng; SHI Youan; YANG Qingtao; ZHOU Ping; ZHAO Shunhong

doi:10.11729/syltlx20190062

Volume 34 Issue 4

Aug. 2020

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Journal of Experiments in Fluid Mechanics > 2020 > 34(4): 87-93. > DOI: 10.11729/syltlx20190062

ZHU Xinxin, LONG Yongsheng, SHI Youan, YANG Qingtao, ZHOU Ping, ZHAO Shunhong. Optimal design of steady enthalpy probe and test verification[J]. Journal of Experiments in Fluid Mechanics, 2020, 34(4): 87-93. DOI: 10.11729/syltlx20190062

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Optimal design of steady enthalpy probe and test verification

1.
Hypervelocity Aerodynamics Institute of China Aerodynamics Research and Development Center, Mianyang Sichuan 621000, China
2.
Computational Aerodynamics Institute of China Aerodynamics Research and Development Center, Mianyang Sichuan 621000, China

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Received Date: May 08, 2019
Revised Date: September 07, 2019

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Abstract

Abstract

For high precision test requirements of the total enthalpy in the ground thermal shielding test of hypersonic vehicles, a kind of steady enthalpy probe with heat shield was developed. The enthalpy probe test system was designed based on the energy balance principle. And the influence of the sampling tube and the cooling water on the enthalpy value was analyzed by FEM. Then the heat insulating structure, water mass flow and gas mass flow were designed and optimized. Finally, the verification test was implemented in the arc heater flow field. The test results show that the design of the enthalpy probe parameter is reasonable, the enthalpy probe structure has a good insulating performance, the repeatability accuracy of the enthalpy probe is better than 2.6%, and the deviation of measurement values of the enthalpy probe and the Fay-Riddell method is less than 13.0%.
- total enthalpy test,
- steady enthalpy probe,
- heat insulating structure,
- optimal design,
- test verification

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