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Performance characteristics of two annular dump diffusers using suction-stabilized vortex flow controlTest results are described for two abrupt area change annular diffusers with provisions for maintaining suction stabilized toroidal vortices at the area discontinuity. Both diffusers had an overall area ratio of 4.0 with the prediffuser area ratio being 1.18 for diffuser A and 1.4 for diffuser B. Performance was evaluated at near atmospheric pressure and temperature for a range of inlet Mach numbers from 0.18 to 0.41 and suction rates from 0 to 18%. Static pressure recovery improved significantly as the suction rate was increased to approximately 11%. Results obtained with diffuser A were superior to that obtained with diffuser B. Flat radial profiles of exit velocity were not obtained since the flow showed preferential hub or tip attachment at moderate suction rates. At high suction rates the diffuser exit flow became circumferentially nonuniform and unstable.
Document ID
19780011114
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
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
January 1, 1978
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-73857
Report Number: NASA-TM-73857
Meeting Information
Meeting: Joint Symp. on Design and Operation of Fluid Machinery
Location: Fort Collins, CO
Country: United States
Start Date: June 12, 1978
End Date: June 14, 1978
Accession Number
78N19057
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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