2022
DOI: 10.1016/j.ijheatmasstransfer.2021.122246
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Velocity measurements in a supersonic wind tunnel with a novel calibration-free seedless velocimetry utilizing laser-induced shockwaves and a double-line probe system

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Cited by 3 publications
(2 citation statements)
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“…Combined with Equation ( 7), the actual time interval between the arrival of the shock wave at the array sensor can be obtained as in Equation (10). (10) ∆t 12 represents the reading error of the time interval when the shock wave passes over sensors 1 and 2, while ∆t 13 represents the reading error of the time interval when the shock wave passes over sensors 1 and 3.…”
Section: Simulationmentioning
confidence: 99%
See 1 more Smart Citation
“…Combined with Equation ( 7), the actual time interval between the arrival of the shock wave at the array sensor can be obtained as in Equation (10). (10) ∆t 12 represents the reading error of the time interval when the shock wave passes over sensors 1 and 2, while ∆t 13 represents the reading error of the time interval when the shock wave passes over sensors 1 and 3.…”
Section: Simulationmentioning
confidence: 99%
“…Predicting, assessing, protecting against, and treating blast-related injuries require accurate data on shock wave pressure; therefore, precise measurement of shock wave pressure values is crucial. Currently, the predominant test methods for effectively acquiring the shock wave pressure parameters include the impact target method, the pressure sensor method, the velocimetry method, and so forth [ 6 , 7 , 8 , 9 , 10 , 11 ]. Although the effect target method is more intuitive, it cannot accurately obtain the shock wave overpressure value [ 12 , 13 ]; however, due to the complex and harsh conditions at the explosion test site, direct pressure sensor measurements are susceptible to additional interferences that may distort the effective signal.…”
Section: Introductionmentioning
confidence: 99%