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A Modified Mixing Length Turbulence Model for Zero and Adverse Pressure GradientsThe modified mixing length (MML) turbulence model was installed in the Proteus Navier-Stokes code, then modified to make it applicable to a wider range of flows typical of aerospace propulsion applications. The modifications are based on experimental data for three flat-plate flows having zero, mild adverse, and strong adverse pressure gradients. Three transonic diffuser test cases were run with the new version of the model in order to evaluate its performance. All results are compared with experimental data and show improvements over calculations made using the Baldwin-Lomax turbulence model, the standard algebraic model in Proteus.
Document ID
19950008193
Acquisition Source
Legacy CDMS
Document Type
Thesis/Dissertation
Authors
Conley, Julianne M.
(NASA Lewis Research Center Cleveland, OH, United States)
Leonard, B. P.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
November 1, 1994
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
E-9220
NASA-TM-106772
NAS 1.15:106772
Report Number: E-9220
Report Number: NASA-TM-106772
Report Number: NAS 1.15:106772
Meeting Information
Meeting: Joint Propulsion Conference
Location: Indianapolis, IN
Country: United States
Start Date: June 27, 1994
End Date: June 29, 1994
Accession Number
95N14607
Funding Number(s)
PROJECT: RTOP 505-62-52
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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