Static Mechanical Properties of 30 × 11.5-14.5, Type VII, Aircraft Tires of Bias-Ply and Radial-Belted Design 871868
An investigation was conducted to determine the static mechanical characteristics of 30 × 11.5 - 14.5 bias-ply and radial aircraft tires. The tires were subjected to vertical and lateral loads and mass moment of inertia tests were conducted. Static load deflection curves, spring rates, hysteresis losses, and inertia data are presented along with a discussion of the advantages and disadvantages of one tire over the other.
Citation: Davis, P. and Lopez, M., "Static Mechanical Properties of 30 × 11.5-14.5, Type VII, Aircraft Tires of Bias-Ply and Radial-Belted Design," SAE Technical Paper 871868, 1987, https://doi.org/10.4271/871868. Download Citation
Author(s):
Pamela A. Davis, Mercedes C. Lopez
Affiliated:
NASA Langley Research Center
Pages: 16
Event:
Aerospace Technology Conference and Exposition
ISSN:
0148-7191
e-ISSN:
2688-3627
Also in:
Aircraft Landing Gear Systems-PT-37, SAE 1987 Transactions: Aerospace-V96-6
Related Topics:
Tires
Aircraft
Springs
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