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Performance of high-area-ratio annular dump diffuser using suction-stabilized-vortex flow controlA short annular dump diffuser having a geometry conductive to formation of suction stabilized toroidal vortices in the region of abrupt area change was tested. The overall diffuser area ratio was 4.0 and the length to inlet height ratio was 2.0. Performance data were obtained at near ambient temperature and pressure for inlet Mach numbers of 0.18 and 0.30 with suction rates ranging from 0 to 18 percent of total inlet mass flowrate. Results show that the exit velocity profile could be readily biased toward either wall by adjustment of inner and outer wall suction rates. Symmetric exit velocity profiles were inherently unstable with a tendency to revert to a hub or tip bias. Diffuser effectiveness was increased from about 38 percent without suction to over 85 percent at a total suction rate of 10 to 12 percent. At the same time diffuser total pressure loss was reduced from 3.1 percent to 1.1 percent at an inlet Mach number of 0.3.
Document ID
19770017196
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Juhasz, A. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Smith, J. M.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
May 1, 1977
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-TM-X-3535
E-9011
Report Number: NASA-TM-X-3535
Report Number: E-9011
Accession Number
77N24140
Funding Number(s)
PROJECT: RTOP 505-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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