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Effect of critical Mach number and flutter on maximum power loading of ducted fans
Document ID
19930081955
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Technical Note
Authors
Regier, Arthur A
Barmby, John G
Hubbard, Harvey H
Date Acquired
August 16, 2013
Publication Date
June 1, 1947
Report/Patent Number
NACA-TN-1330
Report Number: NACA-TN-1330
Accession Number
93R11245
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIR FLOW - WIND TUNNEL FANS
COMPRESSORS - BLADES - VIBRATION
AIR FLOW - COMPRESSORS, AXIAL
BLOWER BLADE
AIRFOILS - NACA 16-012
MACH NUMBER
WIND TUNNEL FANS, AXIAL
LOADS - PROPELLERS
WIND TUNNEL FANS - VIBRATION
FLUTTER
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