Numerical Study of the Three-dimensional Flow Field in Compact Spinning with Inspiratory Groove

In compact spinning with inspiratory groove, the computational fluid dynamic model, computed with parallel technologies and Fluent 6.3, was developed to simulate the flow field in the compact zone with 3D computational fluid dynamic technology. Flowing state, distributions of static pressure and velocity in the compact zone were characterized and analyzed. The results showed that the compact principle of compact spinning with inspiratory groove consists of compact by airflow and compact by the shape of the inspiratory groove, and the static pressure in the condensing zone is negative, as well as the velocity of airflow in the compact zone is not zero. The fluctuation of the static pressure and velocity near the bottom of the inspiratory groove is relatively bigger and the number of the fluctuation is equal to the number of the round holes in the compact zone.