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Development of a Twin-spool Turbofan Engine Simulation Using the Toolbox for Modeling and Analysis of Thermodynamic Systems (T-MATS)The Toolbox for 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
20140016530
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
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, Johathan S.
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
November 21, 2014
Publication Date
July 28, 2014
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
GRC-E-DAA-TN16276
Meeting Information
Meeting: Propulsion and Energy Forum 2014
Location: Cleveland, OH
Country: United States
Start Date: July 28, 2014
End Date: July 30, 2014
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNC10BA16B
CONTRACT_GRANT: NNC12BA01B
WBS: WBS 284848.02.05.03.02.03
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
thermodynamic simulation
numerical simulation
propulsion simulation
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