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A Comparison of Wing Loads Measured in Flight on a Fighter-Type Airplane by Strain-Gage and Pressure Distribution Methods
Document ID
19930082623
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Aiken, William S
Howard, Donald A
Date Acquired
August 16, 2013
Publication Date
November 1, 1949
Report/Patent Number
NACA-TN-1967
Report Number: NACA-TN-1967
Accession Number
93R11913
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FLUTTER - WINGS
PRESSURE DISTRIBUTION - WINGS
PULL-UPS
WINGS - BENDING MOMENTS
LOAD DISTRIBUTION, WING-SPAN
AIRPLANES, FIGHTER
LOADING, WING
STALLING
INSTRUMENTS - STRAIN GAUGES
WIND TUNNEL TESTS - AAL - HIGH-SPEED (16')
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