LAUSR

In this research an experimental system which 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 was used to generate the tail jet. The model shape and the jet rate were all varied to investigate on different flow patterns. Experiments for the cold gas jet were firstly 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.