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Single shaft automotive gas turbine engine characterization testAn automotive gas turbine incorporating a single stage centrifugal compressor and a single stage radial inflow turbine is described. Among the engine's features is the use of wide range variable geometry at the inlet guide vanes, the compressor diffuser vanes, and the turbine inlet vanes to achieve improved part load fuel economy. The engine was tested to determine its performance in both the variable geometry and equivalent fixed geometry modes. Testing was conducted without the originally designed recuperator. Test results were compared with the predicted performance of the nonrecuperative engine based on existing component rig test maps. Agreement between test results and the computer model was achieved.
Document ID
19790023958
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Johnson, R. A.
(Detroit Diesel Allison Indianapolis, IN, United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1979
Subject Category
Urban Technology And Transportation
Report/Patent Number
DDA-EDR-9790
NASA-CR-159654
DOE/NASA/0004-79/1
Report Number: DDA-EDR-9790
Report Number: NASA-CR-159654
Report Number: DOE/NASA/0004-79/1
Accession Number
79N32129
Funding Number(s)
CONTRACT_GRANT: DEN3-4
CONTRACT_GRANT: EC-77-A-31-1040
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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