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Compressor and fan wake characteristicsApproaches for developing an analytical model capable of determining the effects of rotor flow and blade parameters and turbulence properties (i.e. energy, velocity correlations, and length scale) on the rotor wake characteristics and its diffusion properties are discussed. The three-dimensional model will employ experimental measurements, instantaneous velocities, and turbulence properties at various stations downstream from a rotor. A triaxial probe and a rotating conventional probe, which is mounted on a traverse gear operated by two step motors, are to be used for these measurements. The final rotor wake model will be capable of predicting the discrete and broadband noise generated in a fan rotor and of evaluating the aerodynamic losses, efficiency and optimum spacing between a rotor and stator in turbomachinery.
Document ID
19750019238
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Lakshminarayana, B.
(Pennsylvania State Univ. University Park, PA, United States)
Date Acquired
September 3, 2013
Publication Date
July 1, 1975
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-143172
Report Number: NASA-CR-143172
Accession Number
75N27310
Funding Number(s)
CONTRACT_GRANT: NSG-3012
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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