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A Process for the Creation of T-MATS Propulsion System Models from NPSS dataA modular thermodynamic simulation package called the Toolbox for the Modeling and Analysis of Thermodynamic Systems (T-MATS) has been developed for the creation of dynamic simulations. The T-MATS software is designed as a plug-in for Simulink (Math Works, Inc.) and allows a developer to create system simulations of thermodynamic plants (such as gas turbines) and controllers in a single tool. Creation of such simulations can be accomplished by matching data from actual systems, or by matching data from steady state models and inserting appropriate dynamics, such as the rotor and actuator dynamics for an aircraft engine. This paper summarizes the process for creating T-MATS turbo-machinery simulations using data and input files obtained from a steady state model created in the Numerical Propulsion System Simulation (NPSS). The NPSS is a thermodynamic simulation environment that is commonly used for steady state gas turbine performance analysis. Completion of all the steps involved in the process results in a good match between T-MATS and NPSS at several steady state operating points. Additionally, the T-MATS model extended to run dynamically provides the possibility of simulating and evaluating closed loop responses.
Document ID
20150002326
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
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)
Guo, Ten-Huei
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
March 3, 2015
Publication Date
November 1, 2014
Subject Category
Fluid Mechanics And Thermodynamics
Numerical Analysis
Aircraft Propulsion And Power
Report/Patent Number
NASA/TM-2014-218409
E-18987
GRC-E-DAA-TN17334
Meeting Information
Meeting: AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
Location: Cleveland, OH
Country: United States
Start Date: July 28, 2014
End Date: July 30, 2014
Sponsors: American Inst. of Aeronautics and Astronautics, American Society for Electrical Engineers, American Society of Mechanical Engineers, Society of Automotive Engineers, Inc.
Funding Number(s)
CONTRACT_GRANT: NNC12BA01B
WBS: WBS 284848.02.05.03.02.03
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
gas path dynamics
aerothermodynamics
system modeling
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