NASA NTRS · 19930094734
Airplane stability in taxying
Abstract
The 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.
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Anderlik, E. 1932-09-01. Airplane stability in taxying. https://ntrs.nasa.gov/citations/19930094734
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