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Light airplane crash tests at three roll angles
| 题名： | Light airplane crash tests at three roll angles |
| 作者： | Castle, C. B.; Alfaro-Bou, E. |
| 关键词： | accelerometer；ests；light；lane；roll；test；rash；cras；dynamics；parameter |
| 摘要： | Three similar twin engine general aviation airplanes were crash tested at the Langley impact dynamics research facility at 27 m sec and at nominal roll angles of 0 deg, -15 deg, and -30 deg. Other flight parameters were held constant. The test facility, instrumentation, test specimens, and test method are briefly described. Structural damage and accelerometer data for each of the three impact conditions are presented and discussed. |
| 报告类型： | 科技报告 |
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