| タイトル | Dynamics of aircraft antiskid braking systems |
| 本文（外部サイト） | http://hdl.handle.net/2060/19820010330 |
| 著者（英） | Dreher, R. C.; Stubbs, S. M.; Smith, E. G.; Tanner, J. A. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1982-02-01 |
| 言語 | eng |
| 内容記述 | A computer study was performed to assess the accuracy of three brake pressure-torque mathematical models. The investigation utilized one main gear wheel, brake, and tire assembly of a McDonnell Douglas DC-9 series 10 airplane. The investigation indicates that the performance of aircraft antiskid braking systems is strongly influenced by tire characteristics, dynamic response of the antiskid control valve, and pressure-torque response of the brake. The computer study employed an average torque error criterion to assess the accuracy of the models. The results indicate that a variable nonlinear spring with hysteresis memory function models the pressure-torque response of the brake more accurately than currently used models. |
| NASA分類 | AIRCRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 82N18204
L-14788
NASA-TP-1959 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/166955 |
