کد مقاله | کد نشریه | سال انتشار | مقاله انگلیسی | نسخه تمام متن |
---|---|---|---|---|
708512 | 1461104 | 2013 | 4 صفحه PDF | دانلود رایگان |

• This paper analyses a multi-holed Pitot tubes calibration in a low-turbulence wind tunnel.
• Hysteresis was discovered under certain conditions.
• Flow visualization was done in order to find the source of the hysteresis.
• The calibrations dependence on turbulent intensity was determined.
Accurate calibrations of multi-hole Pitot tubes require thousands of measurements spanning ranges of the fluid's velocity, and the pitch and yaw angles. When calibrating a commercially-manufactured multi-hole Pitot tube in NIST's low-turbulence wind tunnel, we found hysteresis in certain ranges of airspeed, pitch angle, and yaw angle. In the worst case, the hysteresis caused a calibration error of 30%. We demonstrate that the hysteresis was caused by a flow instability associated with flow separation. A turbulence intensity of only 1% removes the hysteresis; however, the calibration depends on the turbulence intensity over the entire range of our measurements (0.25–2%). Therefore, multi-hole Pitot tubes should be calibrated and used at the same turbulence levels.
Journal: Flow Measurement and Instrumentation - Volume 33, October 2013, Pages 106–109