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Planar equations of rollout motion for an aircraft with free or steerable landing gearsEquations were derived for an aircraft in a three-point attitude. Transient tire forces were simulated by delaying the application of forces derived from steady-state considerations. Predicted rollout trajectories were similar to those measured in tests of a small-scale landing-gear model equipped with pneumatic tires (where a laterally sloping runway was used to simulate a crosswind), both with and without nose-wheel steering.
Document ID
19820015370
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Sleeper, R. K. (NASA Langley Research Center Hampton, VA, United States)
Smith, E. G. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1982
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-TP-1984
L-11689
NAS 1.60:1984
Report Number: NASA-TP-1984
Report Number: L-11689
Report Number: NAS 1.60:1984
Accession Number
82N23244
Funding Number(s)
PROJECT: RTOP 505-44-33-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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