Abstract This paper presents the results of an investigation of ejectors with the low entrainment ratio. A technique for calculating the ejectors with a curvilinear axis has been developed. Comparative studies of the performance characteristics of ejectors with the rectilinear axis of the mixing chamber and the curvilinear initial section of the mixing chamber are carried out.
Development of the Technique for Calculating the Ejectors with Low Entrainment Ratios
Russian Aeronautics ; 61 , 1 ; 64-70
2018-01-01
7 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Development of the Technique for Calculating the Ejectors with Low Entrainment Ratios
Online Contents | 2018
|An equation for the entrainment of ejectors.
AIAA | 1966
|Entrainment and mixing in thrust augmenting ejectors
AIAA | 1983
|Engineering Index Backfile | 1958
|