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Design and experimental performance of short curved wall diffusers with axial symmetry utilizing slot suctionThe feasibility of designing short curved wall axially symmetrical subsonic diffusers utilizing suction through slots in the diffuser walls to prevent flow separation was investigated. A potential flow analysis was made, and a digital computer program was written for determining the diffuser wall contour for prescribed boundary conditions. The flow field included branch flow so that the suction slot geometry could be a part of the diffuser design. One bell shaped diffuser and three annular diffusers with area ratios of either 2.5:1 or 3:1 were designed, fabricated, and tested. Minimum suction requirements of metastable operation ranged from 6.3 percent to 12 percent when operating with inlet air velocities in the 1000 to 250 ft/sec (30 to 76 m/sec) range. For stable operation suction rates from 10 percent to 22 percent were required. In all cases the diffuser effectiveness was above 95 percent based on the conventional definition, and from 81 percent to 94 percent when the suction loss was accounted for. The exit velocity profiles were virtually flat with no more than + or - 9% variation over 95 percent of the exit area when operated with sufficient suction to prevent flow separation.
Document ID
19730011578
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Yang, T.
(Clemson Univ. SC, United States)
Hudson, W. G.
(Clemson Univ. SC, United States)
Nelson, C. D.
(Clemson Univ. SC, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1973
Publication Information
Publisher: NASA
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-CR-2209
Report Number: NASA-CR-2209
Accession Number
73N20305
Funding Number(s)
CONTRACT_GRANT: NGR-41-001-031
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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