Volume 30 Issue 4
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Zu Xiaoyong, Zhang Lin, Xiao Bin, Zhu Shimin. 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
Citation: Zu Xiaoyong, Zhang Lin, Xiao Bin, Zhu Shimin. 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
shu

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

  • 1.

    China Aerodynamics Reserch and Development Center, Mianyang Sichuan 621000, China

  • 2.

    Chengdu Aero-Instrument Corporation, Chengdu 610091, China

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  • Received Date: January 07, 2016
  • Revised Date: June 27, 2016
    Graphical 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.
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    • References (12)
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