Study and development of total pressure probe and pitot tube in 3m×2m icing wind tunnel

Zu Xiaoyong; Zhang Lin; Xiao Bin; Zhu Shimin

doi:10.11729/syltlx20160006

Volume 30 Issue 4

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Article Navigation > Journal of Experiments in Fluid Mechanics > 2016 > 30(4): 76-80

Zu Xiaoyong, Zhang Lin, Xiao Bin, et al. Study and development of total pressure probe and pitot tube in 3m×2m icing wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2016, 30(4): 76-80. doi: 10.11729/syltlx20160006

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Study and development of total pressure probe and pitot tube in 3m×2m icing wind tunnel

doi: 10.11729/syltlx20160006

1.
China Aerodynamics Reserch and Development Center, Mianyang Sichuan 621000, China
2.
Chengdu Aero-Instrument Corporation, Chengdu 610091, China

Received Date: 2016-01-08
Rev Recd Date: 2016-06-28
Publish Date: 2016-08-25

Abstract

Abstract

The total pressure probe and the pitot tube with the anti-icing/deicing functions are important measurement equipment in icing wind tunnels for which the aerodynamic design is critical. Taking a cue from some airspeed head's manufacture, the total pressure probe and the pitot tube are designed, by using new techniques and deploying the proper heated cable distribution. They show reasonable results in the ground-based static testing, calibration and experiment in the icing wind tunnel with high reliability and insulating property according to China national military standard.
- icing wind tunnel,
- anti-icing/deicing system,
- total pressure probe,
- pitot tube,
- reliability,
- insulating property

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References(12)

References

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