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   Numerical study of mixing enhancement through nanomixers using the throttling approach  
   
نویسنده Darbandi M. ,Sabouri M.
منبع scientia iranica - 2015 - دوره : 22 - شماره : 3-F - صفحه:1306 -1316
چکیده    In this study, we intend to improve the mixing performance of a nanoscale mixer using the throttling idea. the study is conducted at a knudsen number of 0.12, which corresponds to the transitional ow regime. therefore, we have chosen the dsmc method to perform reliable numerical simulations. we consider a number of di erent throttles with various widths and shapes to enrich our study and to explore a wider range of their inuences on the mixing evolution. we choose a linear converging-diverging nozzle profile, an arced converging-diverging nozzle profile, and a sudden contraction-expansion configuration as our throttle shapes. the results show that both the mixing length and the mass ow rate decrease as the throttle widths decrease. however, the decrease in throttle width plays a more effective role in reducing the mixing length than the decrease in mass ow rate. evaluating the results of three chosen throttle shapes, we conclude that the arced nozzle and sudden contraction-expansion shapes result in less mixing length and mass ow rate magnitudes; although the reductions are more pronounced for the latter shape. we also conclude that throttle shape a ects the reduction in mixing length more seriously than the reduction in mass ow rate.
کلیدواژه Nanomixer; Throttling; Mixing length; Mixing ow rate; DSMC method
آدرس sharif university of technology, Centre of Excellence in Aerospace Systems,Institute for Nanoscience and Nanotechnology, Department of Aerospace Engineering, ایران, sharif university of technology, Centre of Excellence in Aerospace Systems, Department of Aerospace Engineering, ایران
 
     
   
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