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Investigation of the effects of inlet shapes on fan noise radiationThe effect of inlet shape on forward radiated fan tone noise directivities was investigated under experimentally simplified zero flow conditions. Simulated fan tone noise was radiated to the far field through various shaped zero flow inlets. Baseline data were collected for the simplest baffled and unbaffled straight pipe inlets. These data compared well with prediction. The more general inlet shapes tested were the conical, circular, and exponential surfaces of revolution and an asymmetric inlet achieved by cutting a straight pipe inlet at an acute angle. Approximate theories were developed for these general shapes and some comparisons with data are presented. The conical and exponential shapes produced directivities that differed considerably from the baseline data while the circular shape produced directivities similar to the baseline data. The asymmetric inlet produced asymmetric directivities with significant reductions over the straight pipe data for some angles.
Document ID
19810014298
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Clark, T. L.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Slotboom, D. R.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Vaidya, P. G.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Date Acquired
September 4, 2013
Publication Date
April 1, 1981
Publication Information
Publisher: NASA
Subject Category
Acoustics
Report/Patent Number
NASA-CR-3416
Report Number: NASA-CR-3416
Accession Number
81N22831
Funding Number(s)
CONTRACT_GRANT: NAS1-15394
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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