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Turbofan forced mixer-nozzle internal flowfield. Volume 1: A benchmark experimental studyAn experimental investigation of the flow field within a model turbofan forced mixer nozzle is described. Velocity and thermodynamic state variable data for use in assessing the accuracy and assisting the further development of computational procedures for predicting the flow field within mixer nozzles are provided. Velocity and temperature data suggested that the nozzle mixing process was dominated by circulations (secondary flows) of a length scale on the order the lobe dimensions which were associated with strong radial velocities observed near the lobe exit plane. The 'benchmark' model mixer experiment conducted for code assessment purposes is discussed.
Document ID
19820014584
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Paterson, R. W.
(United Technologies Research Center East Hartford, CT, United States)
Date Acquired
September 4, 2013
Publication Date
April 1, 1982
Publication Information
Publisher: NASA
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-3492
NAS 1.26:3492
Accession Number
82N22458
Funding Number(s)
PROJECT: RTOP 505-32-12
CONTRACT_GRANT: NAS3-20951
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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