2018
DOI: 10.1088/1742-6596/1065/16/162002
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Dynamic characterisation of pressure transducers using shock tube methods

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Cited by 5 publications
(4 citation statements)
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“…In order to minimize the boundary layer effect on the strength of the generated shock waves, the inner surfaces of the walls of the tube were machined to a mean roughness of less than 0.2 µm. The shock tube is rigidly attached with five massive mounting blocks along its length in order to eliminate the vibrations of the tube generated by the opening of the valve and the motion of the shock waves, which could affect the more acceleration-sensitive pressure meters during calibration [12,22,23]. The complete tube sections were tested at a static pressure of 10 MPa for 30 min to ensure that reliable sealing is maintained under the operating conditions of the shock tube.…”
Section: Developed Diaphragmless Shock Tubementioning
confidence: 99%
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“…In order to minimize the boundary layer effect on the strength of the generated shock waves, the inner surfaces of the walls of the tube were machined to a mean roughness of less than 0.2 µm. The shock tube is rigidly attached with five massive mounting blocks along its length in order to eliminate the vibrations of the tube generated by the opening of the valve and the motion of the shock waves, which could affect the more acceleration-sensitive pressure meters during calibration [12,22,23]. The complete tube sections were tested at a static pressure of 10 MPa for 30 min to ensure that reliable sealing is maintained under the operating conditions of the shock tube.…”
Section: Developed Diaphragmless Shock Tubementioning
confidence: 99%
“…The reflection of the shock front off the endwall of the driven section, where the pressure meter to be calibrated is mounted, causes a rapidly rising step change in the pressure at this point. By assuming a calorically perfect gas and an adiabatic flow, the amplitude of the pressure step upon reflection of the initial shock front can be calculated using traceable measurements of the shock wave velocity W, and the initial, stationary absolute pressure p 1, and temperature T 1 of the gas in the driven section, as [6,[8][9][10][11][12]:…”
Section: Introductionmentioning
confidence: 99%
“…This development has been continuing in the ongoing 17IND07 DynPT-project [5] of the The European Metrology Programme for Innovation and Research (EMPIR). National Physical Laboratory (NPL) and Research Institute of Sweden (RISE) are developing shock tubes [6,7]. Laboratoire national de métrologie et d'essais/Ecole Nationale Supérieure d'Arts et Métiers (LNE/ENSAM) are developing dynamic pressure standards based on shock tube and fast-opening valve principles [1].…”
Section: Introductionmentioning
confidence: 99%
“…The deviation of this output from a perfect step response can be thought of as a measure of the system's non-ideal dynamic characteristics. This paper reports (in more detail than Knott and Robinson, 2018) on the validation of the National Physical Laboratory (NPL)'s shock tube facilities and on how different pressure measurement systems responded to pressure steps generated within them.…”
Section: Introductionmentioning
confidence: 99%