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Airplane stability in taxyingThe stability analysis of an airplane while rolling is much more simplified to the extent that it can be obtained for numerical data which can be put to practical use in the design of landing gear dimensions. Every landing gear type attains to a critical ground friction coefficient that decides the beginning of instability, i.e., nosing over. This study has, in addition, a certain interest for the use of wheel brakes.
Document ID
19930094734
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Anderlik, E
Date Acquired
September 6, 2013
Publication Date
September 1, 1932
Report/Patent Number
NACA-TM-682
Accession Number
93R23654
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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