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Static and yawed-rolling mechanical properties of two type 7 aircraft tires
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | McCarty, J. L. Tanner, J. A. Stubbs, S. M. |
| Copyright Year | 1981 |
| Description | Selected mechanical properties of 18 x 5.5 and 49 x 17 size, type 7 aircraft tires were evaluated. The tires were subjected to pure vertical loads and to combined vertical and lateral loads under both static and rolling conditions. Parameters for the static tests consisted of tire load in the vertical and lateral directions, and parameters for the rolling tests included tire vertical load, yaw angle, and ground speed. Effects of each of these parameters on the measured tire characteristics are discussed and, where possible, compared with previous work. Results indicate that dynamic tire properties under investigation were generally insensitive to speed variations and therefore tend to support the conclusion that many tire dynamic characteristics can be obtained from static and low speed rolling tests. Furthermore, many of the tire mechanical properties are in good agreement with empirical predictions based on earlier research. |
| File Size | 2423063 |
| Page Count | 82 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19810015936 |
| Archival Resource Key | ark:/13960/t8z942b32 |
| Language | English |
| Publisher Date | 1981-05-01 |
| Access Restriction | Open |
| Subject Keyword | Structural Mechanics Landing Gear Aircraft Tires Mechanical Properties Yawing Moments Structural Design Criteria Antiskid Devices Rolling Moments Hysteresis Static Loads Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
