Abstract
A supersonic ejector utilizes the energy and momentum of a primary motive jet to entrain and compress a secondary co-flow. It is a pure aerodynamic device that has no moving parts and the flow is brought about by just gas dynamics of the two flows confined within a variable area duct.
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References
Addy, A.L.: Supersonic Ejector-Diffuser Theory and Experiment (1981)
Srisha Rao, M.V., Jagadeesh, G.: Experimental Investigations on Shock Oscillations and Mixing in a Supersonic Ejector. In: 1st International Conference on High Temperature Gas Dynamics, Beijing, October 15-17 (2012)
Srisha Rao, M.V., Jagadeesh, G.: Visualization and Image Processing of Compressible Flow in a Supersonic Gaseous Ejector. Journal of the Indian Institute of Science 93(1) (2013)
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Rao, M.V.S., Jagadeesh, G. (2015). Mixing in a Supersonic Ejector - An Experimental Investigation. In: Bonazza, R., Ranjan, D. (eds) 29th International Symposium on Shock Waves 2. ISSW 2013. Springer, Cham. https://doi.org/10.1007/978-3-319-16838-8_18
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DOI: https://doi.org/10.1007/978-3-319-16838-8_18
Publisher Name: Springer, Cham
Print ISBN: 978-3-319-16837-1
Online ISBN: 978-3-319-16838-8
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