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Enhancement of the Open National Combustion Code (OpenNCC) and Initial Simulation of Energy Efficient Engine CombustorIn this paper, we present the recent enhancement of the Open National Combustion Code (OpenNCC) and apply the OpenNCC to model a realistic combustor configuration (Energy Efficient Engine (E3)). First, we perform a series of validation tests for the newly-implemented advection upstream splitting method (AUSM) and the extended version of the AUSM-family schemes (AUSM+-up). Compared with the analytical/experimental data of the validation tests, we achieved good agreement. In the steady-state E3 cold flow results using the Reynolds-averaged Navier-Stokes(RANS), we find a noticeable difference in the flow fields calculated by the two different numerical schemes, the standard Jameson- Schmidt-Turkel (JST) scheme and the AUSM scheme. The main differences are that the AUSM scheme is less numerical dissipative and it predicts much stronger reverse flow in the recirculation zone. This study indicates that two schemes could show different flame-holding predictions and overall flame structures.
Document ID
20170001291
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Miki, Kenji
(NASA Glenn Research Center Cleveland, OH, United States)
Moder, Jeffrey
(NASA Glenn Research Center Cleveland, OH United States)
Liou, Meng-Sing
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
February 3, 2017
Publication Date
July 25, 2016
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
GRC-E-DAA-TN34437
Report Number: GRC-E-DAA-TN34437
Meeting Information
Meeting: AIAA/SAE/ASEE Joint Propulsion Conference
Location: Salt Lake City, UT
Country: United States
Start Date: July 25, 2016
End Date: July 27, 2016
Sponsors: American Society for Electrical Engineers, Society of Automotive Engineers, Inc., American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNC12BA01B
WBS: WBS 109492.02.03.01.20
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Combustor-turbine interaction
Hot streaks
Code validation
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