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Beta Testing of CFD Code for the Analysis of Combustion SystemsA preliminary version of OpenNCC was tested to assess its accuracy in generating steady-state temperature fields for combustion systems at atmospheric conditions using three-dimensional tetrahedral meshes. Meshes were generated from a CAD model of a single-element lean-direct injection combustor, and the latest version of OpenNCC was used to calculate combustor temperature fields. OpenNCC was shown to be capable of generating sustainable reacting flames using a tetrahedral mesh, and the subsequent results were compared to experimental results. While nonreacting flow results closely matched experimental results, a significant discrepancy was present between the code's reacting flow results and experimental results. When wide air circulation regions with high velocities were present in the model, this appeared to create inaccurately high temperature fields. Conversely, low recirculation velocities caused low temperature profiles. These observations will aid in future modification of OpenNCC reacting flow input parameters to improve the accuracy of calculated temperature fields.
Document ID
20150023060
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Yee, Emma
(Columbia Univ. New York, NY, United States)
Wey, Thomas
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
December 15, 2015
Publication Date
November 1, 2015
Subject Category
Aeronautics (General)
Computer Programming And Software
Fluid Mechanics And Thermodynamics
Report/Patent Number
E-19150
GRC-E-DAA-TN10745
NASA/TM-2015-218897
Report Number: E-19150
Report Number: GRC-E-DAA-TN10745
Report Number: NASA/TM-2015-218897
Funding Number(s)
WBS: WBS 794072.02.03.05.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Temperature
OpenNCC
CFD
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