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Flight Investigation of the Effect of Transient Wing Response on Measured Accelerations of a Modern Transport Airplane in Rough Air
Document ID
19930082768
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Schufflebarger, C C
Mickleboro, Harry C
Date Acquired
August 16, 2013
Publication Date
August 1, 1950
Report/Patent Number
NACA-TN-2150
Report Number: NACA-TN-2150
Accession Number
93R12058
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ACCELERATIONS
WINGS - STIFFNESS
AIRPLANES, TRANSPORT
WINGS - VIBRATION
LOADS, GUST
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