Article ID Journal Published Year Pages File Type
4452759 Journal of Aerosol Science 2011 13 Pages PDF
Abstract

The flow field and particle transport in supersonic/hypersonic impactors are investigated numerically for a wide range of pressure ratios P0/Pb, nozzle to plate distances L/Dn and nozzle diameters. The results show that in the range of 0.5

Research highlights► In the range of 0.5

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Physical Sciences and Engineering Earth and Planetary Sciences Atmospheric Science
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Numerical investigation of the flow field and cut-off characteristics of supersonic/hypersonic impactors
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