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Static Mechanical Properties of 30 × 11.5-14.5, Type VII, Aircraft Tires of Bias-Ply and Radial-Belted Design
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English
Abstract
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.
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Authors
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.Also In
References
- Cesar, J. P. Musy, J. Olds, R. Development of Radial Aircraft Tires 38th International Air Safety Seminar Boston, Massachusetts November 4-7 1985
- Tanner, J. A. Fore-and-Aft Elastic Response Characteristics of 34 × 9.9, Type VII, 14 Ply-Rating Aircraft Tire of Bias-Ply, Bais-Belted, and Radial-Belted Design 1974
- Tanner, J. A. Stubbs, S. M. McCarty, J. L. Static and Yawed-Rolling Mechanical Properties of Two Type VII Aircraft Tires 1963
- Tanner, J. A. Stubbs, S. M. Dreher, R. C. Smith, E. G. Dynamics of Aircraft Antiskid Braking Systems 1959 February 1982
- Volterra, E. Zachmanoglou, E. C. Dynamics of Vibrations Merrill Books, Inc. 1965 58 60