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Development of a Twin-Spool Turbofan Engine Simulation Using the Toolbox for the Modeling and Analysis of Thermodynamic Systems (T-MATS)The Toolbox for the Modeling and Analysis of Thermodynamic Systems (T-MATS) is a tool that has been developed to allow a user to build custom models of systems governed by thermodynamic principles using a template to model each basic process. Validation of this tool in an engine model application was performed through reconstruction of the Commercial Modular Aero-Propulsion System Simulation (C-MAPSS) (v2) using the building blocks from the T-MATS (v1) library. In order to match the two engine models, it was necessary to address differences in several assumptions made in the two modeling approaches. After these modifications were made, validation of the engine model continued by integrating both a steady-state and dynamic iterative solver with the engine plant and comparing results from steady-state and transient simulation of the T-MATS and C-MAPSS models. The results show that the T-MATS engine model was accurate within 3% of the C-MAPSS model, with inaccuracy attributed to the increased dimension of the iterative solver solution space required by the engine model constructed using the T-MATS library. This demonstrates that, given an understanding of the modeling assumptions made in T-MATS and a baseline model, the T-MATS tool provides a viable option for constructing a computational model of a twin-spool turbofan engine that may be used in simulation studies.

Document ID
20150000858
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Zinnecker, Alicia M.
(N and R Engineering and Management Services Parma Heights, OH, United States)
Chapman, Jeffryes W.
(Vantage Partners, LLC Brook Park, OH, United States)
Lavelle, Thomas M.
(NASA Glenn Research Center Cleveland, OH, United States)
Litt, Jonathan S.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
January 29, 2015
Publication Date
November 1, 2014
Subject Category
Fluid Mechanics And Thermodynamics
Aircraft Propulsion And Power
Computer Programming And Software
Report/Patent Number
NASA/TM-2014-218402
E-18980
GRC-E-DAA-TN17235
Funding Number(s)
WBS: WBS 284848.02.05.03.02.03
CONTRACT_GRANT: NNC12BA01B
CONTRACT_GRANT: NNC10BA16B
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
numerical simulation
thermodynamic simulation
propulsion simulation
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