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Full-scale wind-tunnel tests of a 35 deg swept-wing fighter airplane with a spoiler- slot-deflector lateral control systemWind tunnel tests of swept-wing fighter aircraft with spoiler-slot-deflector lateral control system
Document ID
19650003115
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Scallion, W. I. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
October 26, 1956
Subject Category
Aircraft
Report/Patent Number
NACA-RM-L56D18
Report Number: NACA-RM-L56D18
Accession Number
65N12716
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FIGHTER AIRCRAFT
LATERAL CONTROL
SPOILER-SLOT AILERON

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