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Summary and analysis of data on damping in yaw and pitch for a numbers of airplane models
Document ID
19930081690
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Cotter, William E
Date Acquired
August 16, 2013
Publication Date
May 1, 1946
Report/Patent Number
NACA-TN-1080
Report Number: NACA-TN-1080
Accession Number
93R10980
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
STABILITY
AIRFOILS - NACA 103 - CHARACTERISTICS WING FLAPS
WINGS, RECTANGULAR
AIRPLANES, TAILLESS
DAMPING IN YAW
DAMPING IN PITCH
PROPELLERS - WINDMILLING

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