2020
DOI: 10.1016/j.ast.2020.106302
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Improved traceable measurement of the reflected step pressure in shock tube with the compensation of shock wave attenuation

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Cited by 15 publications
(5 citation statements)
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“…The boundary conditions for this equation take into account that all the boundaries are stationary, except for the wall of the FOV, the velocity of which in the axial direction is constant and negative. After solving (10), the mesh is modified as…”
Section: E Numerical Modelmentioning
confidence: 99%
See 1 more Smart Citation
“…The boundary conditions for this equation take into account that all the boundaries are stationary, except for the wall of the FOV, the velocity of which in the axial direction is constant and negative. After solving (10), the mesh is modified as…”
Section: E Numerical Modelmentioning
confidence: 99%
“…1(c)). The amplitude of the pressure step change upon reflection of the shock front can be calculated as [8], [9], [10]…”
Section: Introductionmentioning
confidence: 99%
“…The reference pressure step signal generated at the end-wall of the driven section is defined by the pressure step amplitude and the arrival time of the initial shock front at the end-wall of the driven section. The amplitude of the generated pressure step at the end-wall of the driven section can be determined using traceable measurements of the shock wave velocity at the end-wall V wall and the initial absolute pressure P 1 and temperature T 1 of the gas in the driven section as [ 22 , 23 ]: where is the adiabatic index, is the shock wave Mach number, is the speed of sound and R 1 is the specific gas constant. The velocity of the shock wave generated in the shock tube attenuates along the driven section due to the thermal-viscous effects [ 24 , 25 , 26 , 27 , 28 , 29 ].…”
Section: Introductionmentioning
confidence: 99%
“…The reference pressure step signal generated at the end-wall of the driven section is defined by the pressure step amplitude and the arrival time of the initial shock front at the end-wall of the driven section. The amplitude of the generated pressure step at the end-wall of the driven section can be determined using traceable measurements of the shock wave velocity at the end-wall V wall and the initial absolute pressure P 1 and temperature T 1 of the gas in the driven section as [22,23]:…”
Section: Introductionmentioning
confidence: 99%
“…Several National Metrology Institutes are working to establish a traceability chain of time-varying pressure measurements [10][11][12][13][14][15]. To establish the traceability, developing the candidate primary standards that can realize time-varying pressure with a specific frequency bandwidth and amplitude is important [16,17]. In addition, developing robust methods for calculating the dynamic response of time-varying pressure measurement systems is needed [18,19].…”
Section: Introductionmentioning
confidence: 99%