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Core compressor exit stage study. Volume 2: Data and performance report for the baseline configurationThe objective of the program is to develop rear stage blading designs that have lower losses in their endwall boundary layer regions. The overall technical approach in this efficiency improvement program utilized General Electric's Low Speed Research Compressor as the principal investigative tool. Tests were conducted in two ways: using four identical stages of blading so that test data would be obtained in a true multistage environment and using a single stage of blading so that comparison with the multistage test results could be made.
Document ID
19810007536
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Wisler, D. C.
(General Electric Co. Cincinnati, OH, United States)
Date Acquired
September 4, 2013
Publication Date
November 1, 1980
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
R80AEG312-VOL-2
NASA-CR-159498
Accession Number
81N16051
Funding Number(s)
CONTRACT_GRANT: NAS3-20070
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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