Article ID Journal Published Year Pages File Type
9702421 Chinese Journal of Aeronautics 2005 6 Pages PDF
Abstract
Three-dimensional numerical computation of the flow fields and pumping performances for the lobed mixer-ejector are conducted using full Navier-Stokes equations. In the computation, the inlet of the primary flow uses the mass flowrate boundary condition. The inlet of the second flow and the out-let of the mixing flow use the pressure boundary condition. Compared with the relative experimental results, it is shown that the present calculation is reasonable. And a series of numerical studies is performed to obtain the effects of area ratio and length-to-diameter ratio of mixing duct on pumping coefficient and thermal mixing efficiency of a lobed mixer-ejector.
Related Topics
Physical Sciences and Engineering Engineering Aerospace Engineering
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