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Low-speed Investigation of the Effect of Small Canard Surfaces on the Directional Stability of a Sweptback-wing Fighter-airplane ModelLow-speed free flight tunnel testing of swept wing fighter aircraft for determining effect of small canard surfaces on directional stability
Document ID
19660024811
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Boisseau, P. C. (NASA Langley Research Center Hampton, VA, United States)
Paulson, J. W. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
August 23, 1956
Subject Category
Aircraft
Report/Patent Number
NACA-RM-L56F19A
Report Number: NACA-RM-L56F19A
Accession Number
66N34101
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LOW SPEED WIND TUNNEL
FIGHTER AIRCRAFT
FREE FLIGHT
SWEPT WING
DIRECTIONAL STABILITY
CANARD

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