2018
DOI: 10.3390/s18103469
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A Flexible Hot-Film Sensor Array for Underwater Shear Stress and Transition Measurement

Abstract: A flexible hot-film sensor array for wall shear stress, flow separation, and transition measurement has been fabricated and implemented in experiments. Parylene C waterproof layer is vapor phase deposited to encapsulate the sensor. Experimental studies of shear stress and flow transition on a flat plate have been undertaken in a water tunnel with the sensor array. Compared with the shear stress derived from velocity profile and empirical formulas, the measuring errors of the hot-film sensors are less than 5%. … Show more

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Cited by 15 publications
(7 citation statements)
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“…If we ignore the spanwise thermal diffusion, assume that the thermal boundary layer is contained within the velocity boundary layer and effects of natural convection are much smaller than forced convection. The relationship between the sensor input power P and shear stress τ w can be expressed as [16,22]:…”
Section: Sensing Principlementioning
confidence: 99%
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“…If we ignore the spanwise thermal diffusion, assume that the thermal boundary layer is contained within the velocity boundary layer and effects of natural convection are much smaller than forced convection. The relationship between the sensor input power P and shear stress τ w can be expressed as [16,22]:…”
Section: Sensing Principlementioning
confidence: 99%
“…The onset and end, as well as 50% intermittent of transition locations can be resolved from the hot-film sensor output [16]. Characterized by the alternating current (AC) output of hot-film sensor, the AC output voltage is stable with very little fluctuation in the laminar boundary layer.…”
Section: Transitionmentioning
confidence: 99%
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“…The intrinsic differences between the boundary layer states include the shear stress at the skin of the airfoil, the heat transfer between the air and the skin, and the increased high frequency pressure fluctuations [1]. Given these differences, various measurement techniques to be used in wind tunnel testing have been developed to determine the local state of the flow around the airfoil, such as pressure or sound transducers [9][10][11], hot film sensors [12][13][14][15], infrared radiation (IR) thermography [16][17][18], and shear stress measurements [19][20][21][22]. Pressure or sound transducers either measure the absolute pressure occurring at discrete locations on an airfoil, or rely on dynamic pressure fluctuations.…”
Section: Introductionmentioning
confidence: 99%
“…The hot-film sensors fabricate on flexible polymer substrate are well fit on curved surfaces with high temporal/spatial resolution and less interference to the flow for in-situ multipoint measurements. Hence, the flexible thermal sensor is a convenient and effective method to determine the shear stress in the boundary layer, both simultaneously and non-intrusively [5].…”
Section: Introductionmentioning
confidence: 99%