2015
DOI: 10.1016/j.flowmeasinst.2014.11.006
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Experimental and numerical investigations of the factors affecting the S-type Pitot tube coefficients

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Cited by 20 publications
(11 citation statements)
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“…The yaw and pitch angle dependence of the S-type Pitot tubes has been investigated by several authors in the past [11][12][13][14]. For the purpose of this paper we use data published in [11] in Figure 4-12 of this reference.…”
Section: ( )mentioning
confidence: 99%
See 1 more Smart Citation
“…The yaw and pitch angle dependence of the S-type Pitot tubes has been investigated by several authors in the past [11][12][13][14]. For the purpose of this paper we use data published in [11] in Figure 4-12 of this reference.…”
Section: ( )mentioning
confidence: 99%
“…One of the most common methods used as the standard reference method (SRM) for flow rate measurement in stacks is the measurement of speed of the gas with S-type Pitot tubes in a grid of points inside the stack [3][4][5]. Accurate measurement using this method is challenging especially when non-axial velocity components are present since the indication of the S-type Pitot tube is sensitive to the orientation of the Pitot head with respect to the gas flow direction [11][12][13][14]. The standards [5,9] describe how to identify and measure the tangential velocity component (swirl) in a stack with the Pitot tube and [3] then introduces a correction for the swirl that is applied if the swirl angle (yaw angle) exceeds 15°.…”
Section: Introductionmentioning
confidence: 99%
“…The uncertainty of the calibration coefficient is one of the major contributions to the overall uncertainty of the the velocity [5]. Thus, the use of a single mean value for C d can have a large effect on the uncertainty of flow rate.…”
Section: Flow Rate Measurement Using Cole Type Pitot Tubementioning
confidence: 99%
“…Another source of error, associated with the use of S-type Pitot tubes and examined in [ 2 ], is due to the inclined gas velocity vectors in presence of non-axial velocity components: the contribution of this error, estimated under the specific conditions simulated in [ 2 ], is up to 2.5%. Measurements were carried out in a wind tunnel, in different experimental conditions and geometries in [ 3 ], yielding similar results.…”
Section: Introductionmentioning
confidence: 99%