Experimental Investigation of the Swirl Development at the Inlet of a Coaxial Rotating Diffuser or Nozzle

摘要

When a fluid enters a rotating pipe, a swirl boundary layer with thickness of δ?Sδ?S appears at the wall and interacts with the axial momentum boundary layer with thickness of δ?δ?. The swirl is produced by the wall shear stress and not due to kinematic reasons as by a turbomachine. In the center of the pipe, the fluid is swirl-free and is accelerated due to axial boundary layer growth. Below a critical flow number Φ?