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Flight Balance For Skin-Friction MeasurementsSkin-friction balance (flight balance) for use in flight on aircraft fuselage incorporates type-one, closed-loop control to make direct skin-friction force measurements. Curved surface element 2 in. (5.08 cm) in diameter used to sense tangential force of airstream passed over it. Linear electromagnetic force motor exerts restoring force that nulls position of sensing element. Applied skin-friction force measured by sensing amount of current through motor necessary to maintain null position. Unit is rugged, accurate, reliable, and easy to operate. Insensitivity of balance to background rectilinear vibrations and ability to sustain large transient loads during takeoffs and landings make it attractive for flight testing.
Document ID
19890000135
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Tcheng, Ping
(NASA Langley Research Center, Hampton, VA.)
Supplee, Frank H., Jr.
(NASA Langley Research Center, Hampton, VA.)
Date Acquired
August 14, 2013
Publication Date
March 1, 1989
Publication Information
Publication: NASA Tech Briefs
Volume: 13
Issue: 3
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LAR-13710
Accession Number
89B10135
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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