Flow field and convective heat transfer of small-scale Taylor-Couette flow induced by end leakage

More and more researchers have paid attention to Taylor-Couette flow whose axial dimension is much larger than other dimensions. However, featured by the limited axial length of the bearing, its flow field and convective heat transfer between the rotator and the stator are highly conglutinated with the leakage at the end of the clearance. An investigation was conducted on the flow field and convective heat transfer of small-scale Taylor-Couette flow induced by end leakage through means of numerical simulation and experimental measurement. The static pressure and temperature of the stator were captured by a micromanometer and a time-resolved infrared camera, respectively. Large Eddy Simulation (LES) was performed to reveal the instantaneous and mean flow field of the shearing flow. Results show that the flow field and convective heat transfer are tightly associated with the presence of end leakage. As approaching the end of the clearance, the flow is dominated by the axial flow induced by the end leakage, and then a series of Taylor vortices gradually distorts and tilts as moving downstream. Along the angular direction, the maximum and minimum static pressures take place near minimum clearance height, respectively. The static pressure along the angular direction and the axial velocity near the minimum clearance height as well as the Nusselt number increase with increases of the rotational Reynolds number and the eccentricity ratio while decreasing with an increase of the dimensionless clearance height. Both natural convection by buoyancy and forced convection by the shearing flow play a significant role in convective heat transfer. Compared with classic Taylor-Couette flow, the occurrence of leakage decreases the maximum static pressure while increasing the minimum static pressure. The formation and evolution of the Taylor vortex are dominated by the axial flow. (c) 2023 Production and hosting by Elsevier Ltd. on behalf of Chinese Society of Aeronautics and Astronautics. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/ licenses/by-nc-nd/4.0/).