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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(Trademark) 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
20150000147
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)
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
Aircraft Propulsion And Power
Numerical Analysis
Report/Patent Number
GRC-E-DAA-TN16306
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: American Society of Mechanical Engineers, Society of Automotive Engineers, Inc., American Inst. of Aeronautics and Astronautics, American Society for Electrical Engineers
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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