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Wind-tunnel Tests of Ailerons at Various Speeds III : Ailerons of 0.20 Airfoil Chord and True Contour with 0.35-aileron-chord Frise Balance on the NACA 23012 Airfoil
Document ID
19930092931
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Kemp, W B
Date Acquired
September 6, 2013
Publication Date
September 1, 1943
Report/Patent Number
NACA-ACR-3I14
NACA-WR-L-325
Report Number: NACA-ACR-3I14
Report Number: NACA-WR-L-325
Accession Number
93R22221
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
CONTROL STICKS - FORCES
FLYING, HIGH-SPEED
AILERONS - WIND TUNNEL TESTS
WIND TUNNEL TESTS - NACA - STABILITY
AIRFOILS - NACA 23012-CHARACTERISTICS
LIFT CURVES - SLOPE
AILERONS, BALANCED - HINGE MOMENTS
AILERONS - BRISTOL FRISE WIND TUNNEL TESTS (NACA-STABILITY)
PRESSURE DISTRIBUTION - AIRFOILS - NACA 23012
MACH NUMBER

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