A Process for the Creation of T-MATS Propulsion System Models from NPSS data
Author(s) -
Jeffryes W. Chapman,
Thomas Lavelle,
Jonathan S. Litt,
Ten-Huei Guo
Publication year - 2014
Publication title -
49th aiaa/asme/sae/asee joint propulsion conference
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2014-3931
Subject(s) - propulsion , process (computing) , computer science , data modeling , systems engineering , software engineering , aerospace engineering , programming language , engineering
A 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.
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