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EFFECT OF HINGE-LINE POSITION ON THE OSCILLATING HINGE MOMENTS AND FLUTTER CHARACTERISTICS OF A FLAP-TYPE CONTROL AT TRANSONIC SPEEDSFree oscillation test to determine hinge moment of trailing-edge, flap control surface with various hinge-line positions at transonic speed
Document ID
19630004887
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Moseley, W. C., Jr. (NASA Langley Research Center Hampton, VA, United States)
Thompson, R. F. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 1, 2013
Publication Date
June 10, 1957
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NACA-RM-L57C11
Report Number: NACA-RM-L57C11
Accession Number
63N14763
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FLUTTER
HINGE MOMENT
FREE OSCILLATION
FLAP CONTROL
TRANSONIC SPEED
TRAILING EDGE

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