Vortex flowmeter

When a fluid moves with high Reynolds number past a stationary object (a “bluff body”), there is a tendency for the fluid to form vortices on either side of the object. Each vortex will form, then detach from the object and continue to move with the flowing gas or liquid, one side at a time in alternating fashion. This phenomenon is known as vortex shedding, and the pattern of moving vortices carried downstream of the stationary object is known as a vortex street

The distance between successive vortices downstream of the stationary object is relatively constant, and directly proportional to the width of the object, for a wide range of Reynolds number values37. If we view these vortices as crests of a continuous wave, the distance between vortices may be represented by the symbol “lambda”.

If a differential pressure sensor is installed immediately downstream of the stationary object in such an orientation that it detects the passing vortices as pressure variations, an alternating signal will be detected.

The frequency of this alternating pressure signal is directly proportional to fluid velocity past the object, since the wavelength is constant. This follows the classic frequency-velocity-wavelength formula common to all traveling waves (λf = v).

Since we know the wavelength will be equal to the bluff body’s width divided by the Strouhal number (approximately 0.17), we may substitute this into the frequency-velocity-wavelength formula to solve for fluid velocity (v) in terms of signal frequency (f) and bluff body width (d).

Thus, a stationary object and pressure sensor installed in the middle of a pipe section constitute a form of flowmeter called a vortex flowmeter. Like a turbine flowmeter with an electronic “pickup” sensor to detect the passage of rotating turbine blades, the output frequency of a vortex flowmeter is linearly proportional to volumetric flow rate.

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If a non-streamline vortex generator (bluff body) is set in the fluid, two rows of regular vortices are alternately generated from both sides of the vortex generator. This type of vortex is called a Karman vortex, as shown in Figure. At the downstream of the vortex generator, alternate and regular vortex rows are formed. Suppose the frequency of the vortex is f, the average velocity of the incoming flow of the measured medium is V, and the width of the front face of the vortex generator is d. According to the Karman vortex street principle, the following relational formula:

f=StV/d Formula (1) where: f-Carman vortex frequency HZ generated on one side of the generator St-Strouhal number (dimensionless number) V-The average flow velocity of fluid (m/s) d-Width of vortex generator (m)

It can be seen that the instantaneous flow can be calculated by measuring the separation frequency of the Karman vortex street. Among them, the Stromhal number (St) is a dimensionless unknown number, Figure (2) shows the relationship between Strouhal number (St) and Reynolds number (Re). In the straight part of the curve table with St=0.17, the release frequency of the vortex is proportional to the flow velocity, which is the measurement range of the vortex flow sensor. As long as the frequency f is detected, the flow velocity of the fluid in the tube can be obtained, and the volume flow rate can be obtained from the flow velocity V. The ratio of the measured pulse number to the volume is called the meter constant (K), see formula (2)
K=3600f/Q(1/m³) Formula (2) where:K = meter constant (m-3). f = number of pulses Q=Volume flow rate (m³)