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NASA One-Dimensional Combustor Simulation--User Manual for S1D_MLThe work presented in this paper is to promote research leading to a closed-loop control system to actively suppress thermo-acoustic instabilities. To serve as a model for such a closed-loop control system, a one-dimensional combustor simulation composed using MATLAB software tools has been written. This MATLAB based process is similar to a precursor one-dimensional combustor simulation that was formatted as FORTRAN 77 source code. The previous simulation process requires modification to the FORTRAN 77 source code, compiling, and linking when creating a new combustor simulation executable file. The MATLAB based simulation does not require making changes to the source code, recompiling, or linking. Furthermore, the MATLAB based simulation can be run from script files within the MATLAB environment or with a compiled copy of the executable file running in the Command Prompt window without requiring a licensed copy of MATLAB. This report presents a general simulation overview. Details regarding how to setup and initiate a simulation are also presented. Finally, the post-processing section describes the two types of files created while running the simulation and it also includes simulation results for a default simulation included with the source code.
Document ID
20140017462
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Stueber, Thomas J.
(NASA Glenn Research Center Cleveland, OH United States)
Paxson, Daniel E.
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
December 17, 2014
Publication Date
October 1, 2014
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-18961
GRC-E-DAA-TN16698
NASA/TM-2014-218387
Funding Number(s)
WBS: WBS 794072.02.03.05.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
combustion
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