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
20170003996
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Miki, Kenji (Georgia Inst. of Tech. Atlanta, GA, United States)
Moder, Jeff (NASA Glenn Research Center Cleveland, OH United States)
Liou, Meng-Sing (NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
April 28, 2017
Publication Date
July 25, 2016
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
GRC-E-DAA-TN34851AIAA Paper 2016-4651Report Number: GRC-E-DAA-TN34851Report Number: AIAA Paper 2016-4651
Meeting Information
Meeting: Joint Propulsion Conference
Location: Salt Lake City, UT
Country: United States
Start Date: July 25, 2016
End Date: July 27, 2016
Sponsors: American Inst. of Aeronautics and Astronautics
IDRelationTitle20170001291See AlsoEnhancement of the Open National Combustion Code (OpenNCC) and Initial Simulation of Energy Efficient Engine Combustor