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Wind-tunnel Tests of a Piston-type Control Booster on an Airfoil and Aileron Model
Document ID
19930092949
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Mendelsohn, Robert A
Date Acquired
September 6, 2013
Publication Date
November 1, 1943
Report/Patent Number
NACA-WR-L-494
NACA-RB-3K15
Accession Number
93R22239
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WIND TUNNEL TESTS - NACA - STABILITY
FLYING, HIGH-SPEED
AILERONS, BALANCED - SEALED-GAP
AILERONS - DEFLECTION
AIRFOILS - NACA 23012
AILERON CONTROLS
AILERONS - HINGE MOMENTS
CONTROLS, SERVO - PISTON

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