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Propulsion System Simulation Using the Toolbox for the Modeling and Analysis of Thermodynamic System T-MATSA simulation toolbox has been developed for the creation of both steady-state and dynamic thermodynamic software models. This paper describes the Toolbox for the Modeling and Analysis of Thermodynamic Systems (T-MATS), which combines generic thermodynamic and controls modeling libraries with a numerical iterative solver to create a framework for the development of thermodynamic system simulations, such as gas turbine engines. The objective of this paper is to present an overview of T-MATS, the theory used in the creation of the module sets, and a possible propulsion simulation architecture. A model comparison was conducted by matching steady-state performance results from a T-MATS developed gas turbine simulation to a well-documented steady-state simulation. Transient modeling capabilities are then demonstrated when the steady-state T-MATS model is updated to run dynamically.
Document ID
20150000150
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Chapman, Jeffryes W.
(Vantage Partners, LLC Brook Park, OH, United States)
Lavelle, Thomas M.
(NASA Glenn Research Center Cleveland, OH United States)
May, Ryan D.
(Vantage Partners, LLC Brook Park, OH, United States)
Litt, Jonathan S.
(NASA Glenn Research Center Cleveland, OH United States)
Guo, Ten-Huei
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
January 5, 2015
Publication Date
July 28, 2014
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
GRC-E-DAA-TN16305
Meeting Information
Meeting: AIAA/ASME/SAE/ASEE Joint Propulsion Conference
Location: Cleveland, OH
Country: United States
Start Date: July 28, 2014
End Date: July 30, 2014
Sponsors: Society of Automotive Engineers, Inc., American Society of Mechanical Engineers, American Society for Electrical Engineers, American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 284848.02.05.03.02.03
CONTRACT_GRANT: NNC12BA01B
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
gas path dynamics
system modeling
aerothermodynamics
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