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Highly loaded multi-stage fan drive turbine-cascade test programTest results are presented for 19 cascades involving five plain and two tandem blade sections. High camber and/or negative reaction is associated with six of the sections. Exit Mach numbers range up to slightly above sonic. Cascade efficiency, exit flow angle and static pressure, and blade surface pressure data are reported with incidence angle, Mach number, solidity, and relative position of the tandem blades as independent variables.
Document ID
19730008051
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Cherry, D. G.
(General Electric Co. Cincinnati, OH, United States)
Staley, T. K.
(General Electric Co. Cincinnati, OH, United States)
Thomas, M. W.
(General Electric Co. Cincinnati, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1973
Publication Information
Publisher: NASA
Subject Category
Propulsion Systems
Report/Patent Number
REPT-72AEG268
NASA-CR-2171
Report Number: REPT-72AEG268
Report Number: NASA-CR-2171
Accession Number
73N16778
Funding Number(s)
CONTRACT_GRANT: NAS3-14304
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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