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A simple method for calculating the characteristics of the Dutch roll motion of an airplaneA simple method for calculating the characteristics of the Dutch roll motion of an airplane is obtained by arranging the lateral equations of motion in such form and order that an iterative process is quickly convergent.
Document ID
19930084655
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Klawans, Bernard B
Date Acquired
August 16, 2013
Publication Date
October 1, 1956
Report/Patent Number
NACA-TN-3754
Report Number: NACA-TN-3754
Accession Number
93R13945
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
DAMPING DERIVATIVES - STABILITY
RESEARCH TECHNIQUE, AERODYNAMICS
STABILITY, LATERAL AND DIRECTIONAL - DYNAMIC

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