| タイトル | Experimental investigation of the cornering characteristics of 18 by 5.5, type 7, aircraft tires with different tread patterns |
| 本文（外部サイト） | http://hdl.handle.net/2060/19750004867 |
| 著者（英） | Dreher, R. C.; Tanner, J. A. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1974-12-01 |
| 言語 | eng |
| 内容記述 | The characteristics, which include the cornering-force and drag-force friction coefficients and self-alining torque, were obtained on dry, damp, and flooded runway surfaces over a range of yaw angles from 0 deg to 12 deg and at ground speeds from approximately 5 to 90 knots. The results indicate that a tread pattern with pinholes in the ribs reduces the tire cornering capability at high yaw angles on a damp surface but improves cornering on a dry surface. A tread pattern which has transverse grooves across the entire width of the tread improves the tire cornering performance slightly at high speeds on the flooded runway surface. The cornering capability of all the tires is degraded at high ground speeds by thin film lubrication and/or tire hydroplaning effects. Alterations to the conventional tread pattern provide only marginal improvements in the tire cornering capability which suggests that runway surface treatments may be a more effective way of improving aircraft ground performance during wet operations. |
| NASA分類 | AIRCRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 75N12939
L-9795
NASA-TN-D-7815 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/191937 |
