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Experiments on identification and control of inflow disturbances in contracting streamsVorticity from all surfaces and isolated objects in the vicinity of the fan intake, including the outside surfaces of the fan housing, were identified as the major sources for disturbances leading to blade passing frequency noise. The previously proposed mechanism based on atmospheric turbulence is refuted. Flow visualization and hot wire techniques were used in three different facilities to document the evolution of various types of disturbances, including the details of the mean flow and turbulence characteristics. The results suggest that special attention must be devoted to the design of the inlet and that geometric modeling may not lead to adequate simulation of the in flight characteristics. While honeycomb type flow manipulators appear to be effective in reducing some of the disturbances, higher pressure drop devices that generate adequate turbulence, for mixing of isolated nonuniformities, may be necessary to suppress the remaining disturbances. The results are also applicable to the design of inlets of open return wind tunnels and similar flow facilities.
Document ID
19830009232
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Lee, A. H.
(Illinois Inst. of Tech. Chicago, IL, United States)
Nagib, H. M.
(Illinois Inst. of Tech. Chicago, IL, United States)
Tan-Atichat, J.
(Illinois Inst. of Tech. Chicago, IL, United States)
Wittwer, D. M.
(Illinois Inst. of Tech. Chicago, IL, United States)
Date Acquired
September 4, 2013
Publication Date
December 1, 1982
Subject Category
Aerodynamics
Report/Patent Number
IIT-FHT-R82-3
NAS 1.26:169831
NASA-CR-169831
Report Number: IIT-FHT-R82-3
Report Number: NAS 1.26:169831
Report Number: NASA-CR-169831
Accession Number
83N17503
Funding Number(s)
CONTRACT_GRANT: NSG-3220
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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