Abstract A mathematical model, which permits the ejector geometry to be optimized, has been designed in the framework of the inverse problem with the use of a non-equilibrium model of the two-phase gas-droplet medium and pressure law. A conventional ejector with a cylindrical chamber and diffuser is compared to the optimum geometry ejector based on numerical studies.
Mixers based on a variable geometry ejector
Russian Aeronautics (Iz VUZ) ; 57 , 3 ; 260-265
2014-07-01
6 pages
Article (Journal)
Electronic Resource
English
Mixers based on a variable geometry ejector
Online Contents | 2014
|Experimental thrust augmentation of variable geometry, two-dimensional, central nozzle ejector
Engineering Index Backfile | 1962
|Experimental thrust augmentation of variable geometry, two-dimensional, central nozzle ejector
Engineering Index Backfile | 1962
|Experimental thrust augmentation of variable geometry, two-dimensional coanda wall jet ejector
Engineering Index Backfile | 1964
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