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Experiments on tandem diffusers with boundary-layer suction applied in betweenExperiments were performed on conical diffusers of various configurations with the same, but rather unusually large, 16:1 area ratio. Because available performance data on diffusers fall short of very large area ratio configurations, an unconventional design, consisting of two diffusers following each other in tandem, was proposed. Both diffusers had the same area ratio of 4:1, but had different taper angles. While for the first diffuser (called leading) the angle remained constant, for the second (called follower), the taper angle was stepped up to higher values. Boundary layer control, by way of suction, was applied between the diffusers, and a single slot suction ring was inserted between them. The leading diffuser had an enclosed nominal divergence angle 2 theta = 5 degrees, while the follower diffusers had either 10, 20, 30, or 40 degrees, respectively, giving 4 combinations. The experiments were performed at four different Reynolds numbers with various suction rates. The rates indicate a general improvement in the performance of all diffusers with boundary layer suction. It appears that the improvement of the pressure recovery depends on both the Reynolds number and the suction rate, and the largest increase, 0.075, was found at the lowest R sub e when the follower divergence was 2 theta = 40 degrees.
Document ID
19790009632
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Barna, P. S.
(Old Dominion Univ. Norfolk, VA, United States)
Date Acquired
September 3, 2013
Publication Date
February 1, 1979
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-158957
Report Number: NASA-CR-158957
Accession Number
79N17803
Funding Number(s)
CONTRACT_GRANT: NAS1-14193
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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