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Short efficient ejector systemsA research program was conducted to improve the performance of low pressure ratio ejector systems. The results show that short, efficient ejectors operating at nearly ideal performance are possible through the use of forced mixer lobes. Forced mixer lobes generate large scale axial vorticity which results in rapid mixing and improved diffuser performance. Ejector testing was conducted using both an ejector wind tunnel. Numerous mixer lobe variations were tested to develop lobe design guidelines. The improved performance of mixer-ejectors is presented over a range of operating conditions. Results of mixer lobe angle, penetration, and alignment are presented. Lobe angles of up to 25 deg, coupled with diffuser wall angles over 20 deg, operate without separation, allowing efficient, short ejector systems. Both warm and cold flow test results are presented. Temperature similarity expressions previously developed are further formulated and verified.
Document ID
19870057965
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Presz, Walter M., Jr.
(United Technologies Research Center East Hartford, CT; Western New England College, Springfield, M, United States)
Morin, Bruce L.
(United Technologies, Research Center East Hartford, CT, United States)
Blinn, Roger F.
(United Technologies Research Center East Hartford, CT, United States)
Date Acquired
August 13, 2013
Publication Date
June 1, 1987
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AIAA PAPER 87-1837
Accession Number
87A45239
Funding Number(s)
CONTRACT_GRANT: NAG3-610
Distribution Limits
Public
Copyright
Other

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