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NASA Lewis Stirling engine computer code evaluationIn support of the U.S. Department of Energy's Stirling Engine Highway Vehicle Systems program, the NASA Lewis Stirling engine performance code was evaluated by comparing code predictions without engine-specific calibration factors to GPU-3, P-40, and RE-1000 Stirling engine test data. The error in predicting power output was -11 percent for the P-40 and 12 percent for the Re-1000 at design conditions and 16 percent for the GPU-3 at near-design conditions (2000 rpm engine speed versus 3000 rpm at design). The efficiency and heat input predictions showed better agreement with engine test data than did the power predictions. Concerning all data points, the error in predicting the GPU-3 brake power was significantly larger than for the other engines and was mainly a result of inaccuracy in predicting the pressure phase angle. Analysis into this pressure phase angle prediction error suggested that improvements to the cylinder hysteresis loss model could have a significant effect on overall Stirling engine performance predictions.
Document ID
19890015370
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Sullivan, Timothy J.
(Sverdrup Technology, Inc. Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1989
Subject Category
Energy Production And Conversion
Report/Patent Number
NASA-CR-182248
NAS 1.26:182248
DOE/NASA/4105-4
E-4580
Report Number: NASA-CR-182248
Report Number: NAS 1.26:182248
Report Number: DOE/NASA/4105-4
Report Number: E-4580
Accession Number
89N24741
Funding Number(s)
CONTRACT_GRANT: DE-AI01-85CE-50112
CONTRACT_GRANT: NAS3-24105
PROJECT: RTOP 778-35-13
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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