2011
DOI: 10.1016/j.proci.2010.06.152
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Pressure loading of detonation waves through 90-degree bend in high pressure H2–O2–N2 mixtures

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Cited by 12 publications
(9 citation statements)
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“…The maximum overpressures and velocities obtained from Figure 2 and 3 were 8-11 barg and 300-600 m/s, respectively. As mentioned earlier, the high compression effect was observed at the end of the pipe (straight pipe), thus, it can be said that the steep pressure rise (detonationlike) was affected by the strong interaction between the hot flame and reflected shock/acoustic wave, due to the highly compressed flame front [22,27]. The condition occurs when an initially laminar flame is hit head-on by the shock waves, producing a sudden release of pressure [22].…”
Section: Overpressure Along Pipementioning
confidence: 92%
See 1 more Smart Citation
“…The maximum overpressures and velocities obtained from Figure 2 and 3 were 8-11 barg and 300-600 m/s, respectively. As mentioned earlier, the high compression effect was observed at the end of the pipe (straight pipe), thus, it can be said that the steep pressure rise (detonationlike) was affected by the strong interaction between the hot flame and reflected shock/acoustic wave, due to the highly compressed flame front [22,27]. The condition occurs when an initially laminar flame is hit head-on by the shock waves, producing a sudden release of pressure [22].…”
Section: Overpressure Along Pipementioning
confidence: 92%
“…The condition occurs when an initially laminar flame is hit head-on by the shock waves, producing a sudden release of pressure [22]. This release sends a strong rarefaction wave to propagate back into the unburned gases, that creates an unburned gas jet, penetrating the burned gas and developing the shear layers, subsequently produces an extreme turbulence that causes a sudden increase in the burning rate whereby 'trains' of compressed waves are formed [22,27]. A study by Karlovitz et al, [28] suggested that the wrinkling of the flame front (turbulisation) can be so great, such that the pockets of trapped unburned gas preheat and collapse in a strong reaction burst.…”
Section: Overpressure Along Pipementioning
confidence: 99%
“…The results showed that obstacles promoted the acceleration of hydrogen flame in the experimental pipe section. In terms of pipe structure, Uchida et al [7] studied the influence of explosion wave on the internal pressure of pipeline in 90° elbow, and the results determined that the pressure load of elbow in two positions was greater than that of straight pipe. One is the peak pressure at the outer edge of the bend due to compression.…”
Section: Introductionmentioning
confidence: 99%
“…Edwards [19] studied the shock wave propagation in 90-degree bend by experiment and points out the relationship between the shock wave velocity and the curvature of the pipe. Frolov [20,21] investigated the detonation wave propagation characteristics of the U-bend tubes by experiment and numerical simulation Uchida [22] explored a comparative study on detonation wave propagation in 90 • straight tube and bend and points out two locations in pipe where pressure values are greater than those in the straight tube. One location is in the outer wall surface of bend and the other appears in the downstream of the bend exit because of the effect of transverse waves.…”
Section: Introductionmentioning
confidence: 99%