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Single stage experimental evaluation of slotted rotor and stator blading, part 9 Final reportSlotted axial flow compressor rotor and slotted stator tests of slot effect on performance of highly loaded blades
Document ID
19680024926
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Rockenbach, R. W. (Pratt and Whitney Aircraft West Palm Beach, FL, United States)
Date Acquired
August 4, 2013
Publication Date
September 26, 1968
Subject Category
Aerodynamics
Report/Patent Number
PWA-FR-2289, PT. 9
NASA-CR-54553
Accession Number
68N34398
Funding Number(s)
CONTRACT_GRANT: NAS3-7603
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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