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Effect of wall suction on performance of a short annular diffuser at inlet Mach numbers up to 0.5A short annular diffuser equipped with wall bleed (suction)capability was evaluated at inlet Mach numbers of 0.186 to 0.5. The diffuser had an area ratio of 4.0 and a length-to-inlet height ratio of 1.6. Test results show that the exit velocity profiles, typical of annular jet flow without suction, could be considerably flattened by application of wall suction. This improved performance was also reflected in diffuser effectiveness (static-pressure recovery) and total-pressure loss results. At the inlet Mach number of 0.5 diffuser static-pressure recovery is equal to or better than at lower inlet Mach numbers for comparable suction rates.
Document ID
19750024928
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Juhasz, A. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
October 1, 1975
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-3302
E-8393
Report Number: NASA-TM-X-3302
Report Number: E-8393
Accession Number
75N33001
Funding Number(s)
PROJECT: RTOP 505-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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