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High Fidelity System Simulation of Multiple Components in Support of the UEET ProgramThe High Fidelity System Simulation effort has addressed various important objectives to enable additional capability within the NPSS framework. The scope emphasized High Pressure Turbine and High Pressure Compressor components. Initial effort was directed at developing and validating intermediate fidelity NPSS model using PD geometry and extended to high-fidelity NPSS model by overlaying detailed geometry to validate CFD against rig data. Both "feedforward" and feedback" approaches of analysis zooming was employed to enable system simulation capability in NPSS. These approaches have certain benefits and applicability in terms of specific applications "feedback" zooming allows the flow-up of information from high-fidelity analysis to be used to update the NPSS model results by forcing the NPSS solver to converge to high-fidelity analysis predictions. This apporach is effective in improving the accuracy of the NPSS model; however, it can only be used in circumstances where there is a clear physics-based strategy to flow up the high-fidelity analysis results to update the NPSS system model. "Feed-forward" zooming approach is more broadly useful in terms of enabling detailed analysis at early stages of design for a specified set of critical operating points and using these analysis results to drive design decisions early in the development process.
Document ID
20060012153
Acquisition Source
Glenn Research Center
Document Type
Contractor Report (CR)
Authors
Plybon, Ronald C.
(General Electric Aircraft Engines Cincinnati, OH, United States)
VanDeWall, Allan
(General Electric Aircraft Engines Cincinnati, OH, United States)
Sampath, Rajiv
(General Electric Global Research Niksayuna, NY, United States)
Balasubramaniam, Mahadevan
(General Electric Global Research Niksayuna, NY, United States)
Mallina, Ramakrishna
(General Electric Global Research Niksayuna, NY, United States)
Irani, Rohinton
(General Electric Global Research Niksayuna, NY, United States)
Date Acquired
September 7, 2013
Publication Date
April 1, 2006
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
NASA/CR-2006-214230
E-15477
Report Number: NASA/CR-2006-214230
Report Number: E-15477
Funding Number(s)
WBS: WBS 984754.02.07.03
CONTRACT_GRANT: NAS3-01135
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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