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The evolution of secondary flow phenomena and their effect on primary shock conditions in shock tubes: Experimentation and numerical model

Fig 9

Experimentally observed shock curvature.

The arrival times of the shock wave normalized with the shock arrival at the H1 sensor showed a curvature of the shock front at the measurement locations (A) O1, (B) O2, (C) O3, and (D) O4.

Fig 9

doi: https://doi.org/10.1371/journal.pone.0227125.g009