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Evaluation of a new concept for reducing free-stream turbulence in wind tunnelsThe feasibility of using a 45 deg-honeycomb for improving the flow quality in wind tunnels was investigated. The results of the experiments indicate that the turbulence levels in a wind tunnel using the 45 deg-honeycomb would be comparable to those obtainable using a conventional honeycomb, i.e., a honeycomb which is positioned normal to the mean flow in the settling chamber. However, this is true only when a 45 deg-screen is mounted immediately downstream of the honeycomb, and when some distance is provided between the trailing edges of the corner turning vanes and the upstream side of the 45 deg-honeycomb. This distance is required for adequate decay of the turning-vane wakes, thereby providing a reasonably uniform mean flow entering the honeycomb. Results demonstrate that this distance should be at least twice the spacing between the turning vanes. Even though the resulting turbulence intensity is the same downstream of both the 45 deg-honeycomb and the conventional honeycomb, there would have to be a significant improvement in the test-section turbulence intensity using the 45 deg-honeycomb to justify the additional expense in fabricating and installing this type of honeycomb.
Document ID
19790025269
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Wigeland, R. A.
(Illinois Inst. of Tech. Chicago, IL, United States)
Tan-Atichat, J.
(Illinois Inst. of Tech. Chicago, IL, United States)
Nagib, H. M.
(Illinois Inst. of Tech. Chicago, IL, United States)
Date Acquired
September 3, 2013
Publication Date
October 1, 1979
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
R79-1
NASA-CR-3196
Report Number: R79-1
Report Number: NASA-CR-3196
Accession Number
79N33440
Funding Number(s)
CONTRACT_GRANT: NSG-1451
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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