首页 | 本学科首页   官方微博 | 高级检索  
     


Performance of Kenics static mixer over a wide range of Reynolds number
Authors:Vimal Kumar  Vaibhav Shirke  KDP Nigam  
Affiliation:aDepartment of Chemical Engineering, Indian Institute of Technology, Delhi, Hauz Khas, New Delhi 110016 India
Abstract:The present study deals with the numerical simulation of flow patterns and mixing behaviour in Kenics static mixer over a wide range of Reynolds number. Three different sets of Kenics mixer (aspect ratio = 1.5) comprised of 3, 9 and 25 elements each have been characterized. The Reynolds number was varied in the range of 1 to 25,000 (i.e., from laminar to turbulent flow regime). The numerical approach takes into account the aspects of the fluid flow at higher Reynolds number values including circumferential velocity profiles at different cross-sections within the Kenics mixer, which were neglected in previous studies. It was observed that cross-sectional mixing in the turbulent flow regime takes place up to 30% of each element length at element-to-element transition; beyond that velocity profiles were uniform. The experiments were also carried out to measure the circumferential and axial velocity profiles and pressure drop in three different Kenics Mixers using air as fluid. The pressure drop per unit element (ΔP/η) was found to be independent of the number of Kenics mixing elements used in the system. The total pressure drop across Kenics mixer obtained by CFD simulations were compared with the experimental pressure drop values and correlations available in the literature. The numerical results were found in good agreement with the experimental as well as the results reported in the literature. A new pressure drop correlation in the Kenics static mixer has been developed.
Keywords:Kenics static mixer  Motionless mixers  CFD  Circumferential and axial velocity profiles  Laminar flow  Turbulence flow  k  ω   model  k  sciencedirect  com/scidirimg/entities/25b   model" target="_blank">gif" alt="var epsilon" title="var epsilon" border="0"> model
本文献已被 ScienceDirect 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号