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Axial-flow fan and compressor blade design data on 52.5 degrees stagger and further verification of cascade data by rotor tests
Document ID
19930081874
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Bogdonoff, Seymour M
Hess, Eugene E
Date Acquired
August 16, 2013
Publication Date
April 1, 1947
Report/Patent Number
NACA-TN-1271
Report Number: NACA-TN-1271
Accession Number
93R11164
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIRFOILS - NACA 65-410
COMPRESSORS, AXIAL
COMPRESSORS - BLADES - CASCADES
LOW DRAG BLOWER BLADE
BLOWERS, AXIAL
AIRFOILS - NACA 65-(12)10
AIRFOILS - NACA 65-810
AIRFOILS - NACA 65-710
AIR FLOW - AIRFOILS - CASCADES
AIRFOILS - NACA 65-(11)10

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