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Quasi-Static and Dynamic Response Characteristics of F-4 Bias-Ply and Radial-Belted Main Gear TiresAn investigation was conducted at Langley Research Center to determine the quasi-static and dynamic response characteristics of F-4 military fighter 30x11.5-14.5/26PR bias-ply and radial-belted main gear tires. Tire properties were measured by the application of vertical, lateral, and fore-and-aft loads. Mass moment-of-inertia data were also obtained. The results of the study include quasi-static load-deflection curves, free-vibration time-history plots, energy loss associated with hysteresis, stiffness and damping characteristics, footprint geometry, and inertia properties of each type of tire. The difference between bias-ply and radial-belted tire construction is given, as well as the advantages and disadvantages of each tire design. Three simple damping models representing viscous, structural, and Coulomb friction are presented and compared with the experimental data. The conclusions discussed contain a summary of test observations.
Document ID
19970026102
Acquisition Source
Langley Research Center
Document Type
Technical Publication (TP)
Authors
Davis, Pamela A.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1997
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
L-17433
NAS 1.60:3586
NASA-TP-3586
Report Number: L-17433
Report Number: NAS 1.60:3586
Report Number: NASA-TP-3586
Accession Number
97N25451
Funding Number(s)
PROJECT: RTOP 505-63-10-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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