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Investigation of the effect of nozzle shape on supersonic/hypersonic impactors designed for size discrimination of nanoparticles
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作者 Saeideh Saadabadi Omid Abouali +1 位作者 Homayoon Emdad Goodarz Ahmadi 《Particuology》 SCIE EI CAS CSCD 2014年第5期60-68,共9页
In this study the flow field and the nanoparticle collection efficiency of supersonic/hypersonic impactors with different nozzle shapes were studied using a computational modeling approach. The aim of this study was t... In this study the flow field and the nanoparticle collection efficiency of supersonic/hypersonic impactors with different nozzle shapes were studied using a computational modeling approach. The aim of this study was to develop a nozzle design for supersonic]hypersonic impactors with the smallest possible cut-off size d5o and rather sharp collection efficiency curves. The simulation results show that the changes in the angle and width of a converging nozzle do not alter the cut-off size of the impactor; however, using a conical Laval nozzle with an L]Dn ratio less than or equal to 2 reduced d5o. The effect of using a cap as a focuser in the nozzle of a supersonic/hypersonic impactor was also investigated. The results show that adding a cap in front of the nozzle had a noticeable effect on decreasing the cut-off size of the impactor. Both fiat disks and conical caps were examined, and it was observed that the nozzle with the conical cap had a lower cut-off size. 展开更多
关键词 Supersonic/hypersonic Impactor Nanoparticle nozzle
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