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The Effects of Static Margin and Rotational Damping in Pitch on the Longitudinal Stability Characteristics of an Airplane as Determined by Tests of a Model in the NACA Free-Flight Tunnel
Document ID
19930092549
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Paulson, John W
Date Acquired
September 6, 2013
Publication Date
June 1, 1944
Report/Patent Number
NACA-WR-L-55
NACA-ARR-L4F02
Report Number: NACA-WR-L-55
Report Number: NACA-ARR-L4F02
Accession Number
93R21839
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
STABILITY, LONGITUDINAL
DAMPING IN PITCH
PITCHING

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