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An Investigation Regarding the Effects of Volume Dynamics on Gas Turbine Engine Performance and OperabilityThis work explores the impact of adding volume dynamics to an electrified turbofan engine model. The zero-dimensional single-input single-output volume elements capture the physics of fluid compressibility of flow in the engine core gas path turbomachinery during transient operation with greater fidelity. Some background regarding the motivation for this effort is provided. A model of the volume element is developed from first principles. The baseline engine model is described and an explanation is given of the modifications made to incorporate the volume elements into the new model. Details of the simulated inputs, designed to elicit exaggerated dynamic responses and to facilitate comparison between the baseline and modified engine models, are explicated. The results of these simulations are presented and discussed, demonstrating that the transient performance and operability of the modified engine model, measured by parameters such as shaft speeds, thrust, and high-pressure compressor (HPC) stall margin, are impacted by the additional dynamics. Commentary is provided regarding potential explanations for the differences in behavior exhibited by the two models. Finally, suggestions are offered for future work that might improve the volume models developed in this effort and leverage the improved fidelity enabled by the modeling of turbomachinery volume dynamics.
Document ID
20260000440
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Nolan M LaMarche
(HX5, LLC)
Thomas M Lavelle
(Glenn Research Center Cleveland, United States)
Jeffryes W Chapman
(Glenn Research Center Cleveland, United States)
Date Acquired
January 14, 2026
Publication Date
January 1, 2026
Publication Information
Subject Category
Aeronautics (General)
Aircraft Propulsion and Power
Report/Patent Number
NASA/TM-20260000440
E20409
Funding Number(s)
WBS: 361807.02.03.03.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
Volume dynamics
modeling
simulation
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