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Wind tunnel investigation of longitudinal aerodynamic characteristics of a powered four-duct-propeller VTOL model in transitionWind tunnel stability tests of longitudinal aerodynamic characteristics of powered four-duct propeller VTOL model in transition
Document ID
19660013630
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Spreemann, K. P. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1966
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-3192
Report Number: NASA-TN-D-3192
Accession Number
66N22919
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
PROPELLER
WIND TUNNEL STABILITY TEST
AERODYNAMIC CHARACTERISTICS
VTOL AIRCRAFT
LONGITUDINAL STABILITY

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