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Highly loaded multi-stage fan drive turbine: Performance of final three configurationsResults for a three-stage highly loaded fan drive turbine follow-on test program are presented. The effects of combinations of tandem and leaned bladerows on three-stage turbine performance were tested. The three-stage turbine with a tandem stator in stage two exhibited a total-to-total efficiency of approximately 0.887 as compared to 0.886 for the plain blade turbine base case.
Document ID
19750002017
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Cherry, D. G. (General Electric Co. Cincinnati, OH, United States)
Thomas, M. W. (General Electric Co. Cincinnati, OH, United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1974
Publication Information
Publisher: NASA
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
GE73AEG481
NASA-CR-2446
Report Number: GE73AEG481
Report Number: NASA-CR-2446
Accession Number
75N10089
Funding Number(s)
CONTRACT_GRANT: NAS3-14304
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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