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Effects of axisymmetric contractions on turbulence of various scalesDigitally acquired and processed results from an experimental investigation of grid generated turbulence of various scales through and downstream of nine matched cubic contour contractions ranging in area ratio from 2 to 36, and in length to inlet diameter ratio from 0.25 to 1.50 are reported. An additional contraction with a fifth order contour was also utilized for studying the shape effect. Thirteen homogeneous and nearly isotropic test flow conditions with a range of turbulence intensities, length scales and Reynolds numbers were generated and used to examine the sensitivity of the contractions to upstream turbulence. The extent to which the turbulence is altered by the contraction depends on the incoming turbulence scales, the total strain experienced by the fluid, as well as the contraction ratio and the strain rate. Varying the turbulence integral scale influences the transverse turbulence components more than the streamwise component. In general, the larger the turbulence scale, the lesser the reduction in the turbulence intensity of the transverse components. Best agreement with rapid distortion theory was obtained for large scale turbulence, where viscous decay over the contraction length was negligible, or when a first order correction for viscous decay was applied to the results.
Document ID
19800023821
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Tan-Atichat, J.
(Illinois Inst. of Tech. Chicago, IL, United States)
Nagib, H. M.
(Illinois Inst. of Tech. Chicago, IL, United States)
Drubka, R. E.
(Illinois Inst. of Tech. Chicago, IL, United States)
Date Acquired
September 4, 2013
Publication Date
September 1, 1980
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-165136
R80-1
Report Number: NASA-CR-165136
Report Number: R80-1
Accession Number
80N32328
Funding Number(s)
CONTRACT_GRANT: NSG-3220
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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