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The Starting Behaviour of a Supersonic Ejector Equipped with a Converging-Diverging Diffuser  

Park GeunHong (한국과학기술원 항공우주공학과)
Kim SeHoon (한국과학기술원 항공우주공학과)
Jin JungKun (한국과학기술원 항공우주공학과)
Kwon SeJin (한국과학기술원 항공우주공학과)
Publication Information
Journal of the Korean Society of Propulsion Engineers / v.9, no.2, 2005 , pp. 70-77 More about this Journal
Abstract
An axisymmetric supersonic ejector equipped with a converging-diverging diffuser was built and pressure at various locations along the ejector-diffuser system was recorded with emphasis on the supersonic starting of the secondary flow. In order to find the effects of the opening size of the secondary flow, a number of openings were used with a constant primary pressure. Supersonic starting was possible only for d/D, the ratio of the opening diameter and the diffuser throat diameter, less than 0.306. for larger values of d/D, the ejection begins at subsonic secondary flow condition. With the closure of the opening, the primary flow brings the normal shock downstream of the converging-diverging diffuser And the starting of the ejector continues even after the closure was removed.
Keywords
Supersonic Ejector; Hysteresis;
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