Jet-supercavity interaction and instability mechanism analysis

In this research, an experimental system that couples the supercavity and the tail jet was established, aiming at exploring on the cavity instability mechanism. Both high pressure gas tank and solid rocket motor were used to generate the tail jet. The model shape and the jet rate were all varied to investigate different flow patterns. Experiments for the cold gas jet were first carried out, obtaining the variation of the flow pattern with the jet strength and the relative location. With strong jet intensity, the supercavity could lose instability by the re-entrained liquid jet, which was mainly generated by the back attack of the tail jet. Furthermore, the effect of the rearward facing step structure on the cavity instability was investigated, validating that the re-entrained jet could be successfully suppressed by this structure. However, when the cavity contacts with the wall surface, another kind of instability induced by cavity/body interaction could be induced. Subsequently, experiments were carried out for the hot jet generated by the solid rocket motor. A new kind of cavity instability at the moment of ignition was observed. The cavity shrinking and collapse processes were compared between different cases. When the ignition process finished, the hot jet transited into a continuous free expansion mode with weak entrainment of liquid. Finally, the cavity instability mechanisms were summarized and compared. Spectral analysis was carried out for different cases. An obvious larger Strouhal number exists for the pressure pulse induced instability.

Automated summary

An experimental system coupling the supercavity and the tail jet was established to study the cavity instability mechanism. The shapes and rates of the model and jet were changed to investigate different flow patterns. The results showed that the supercavity could lose instability due to the re-entrained liquid jet produced by the tail jet. The rearward facing step structure successfully suppressed the re-entrained jet, but cavity/body interaction induced another type of instability. New cavity instability was observed at ignition with hot jet generated by the solid rocket motor. The cavity instability mechanisms were summarized and compared, with spectral analysis showing larger Strouhal number for pressure pulse induced instability.