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Wind-tunnel test of a full-scale, 1.1 pressure ratio, ducted lift-cruise fanFixed blade angle, ducted, tip-turbine-driven, cruise fan as aircraft propulsive device at high subsonic speed
Document ID
19650000800
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Biggers, J. C. (NASA Ames Research Center Moffett Field, CA, United States)
Corsiglia, V. R. (NASA Ames Research Center Moffett Field, CA, United States)
Giulianetti, D. J. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1964
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-2498
Report Number: NASA-TN-D-2498
Accession Number
65N10401
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SUBSONIC SPEED
TURBINE BLADE
SUBSONIC WIND TUNNEL
DUCTED FAN

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