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Initial development of the two-dimensional ejector shear layer - Experimental resultsAn experimental investigation designed to study the development of shear layers in a two-dimensional single-nozzle ejector has been completed. In this study, combinations of air/air, argon/air, helium/air, and air/helium were used as the supersonic primary and subsonic secondary, respectively. Mixing of the gases occurred in a constant-area tube 39.1 mm high by 25.4 mm wide, where the inlet static pressure was maintained at 35 kPa. The cases studied resulted in convective Mach numbers between 0.058 and 1.64, density ratios between 0.102 and 3.49, and velocity ratios between 0.065 and 0.811. The resulting data shows the differences in the shear-layer development for the various combinations of independent variables utilized in the investigation. The normalized growth-rates in the near-field were found to be similar to two-dimensional mixing layers. These results have enhanced the ability to analyze and design ejector systems as well as providing a better understanding of the physics.
Document ID
19930066195
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Benjamin, M. A.
(NASA Lewis Research Center Cleveland, OH, United States)
Dufflocq, M.
(NASA Lewis Research Center Cleveland, OH, United States)
Roan, V. P.
(Florida Univ. Gainesville, United States)
Date Acquired
August 16, 2013
Publication Date
June 1, 1993
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AIAA PAPER 93-2440
Meeting Information
Meeting: AIAA, SAE, ASME, and ASEE, Joint Propulsion Conference and Exhibit
Location: Monterey, CA
Country: United States
Start Date: June 28, 1993
End Date: June 30, 1993
Sponsors: SAE, ASEE, ASME, AIAA
Accession Number
93A50192
Funding Number(s)
CONTRACT_GRANT: NAG3-1187
Distribution Limits
Public
Copyright
Other

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