【24h】

Effect of Shock Pulse Load on the Ice Cover During Landing of an Airplane

机译:飞机着陆过程中冲击脉冲载荷对冰盖的影响

获取原文

摘要

The paper presents deflections of the ice cover caused by the combinedaction of the shock load and the subsequent deceleration movementload during airplane landing. The influence of shock load and thethickness of ice cover on the possibility of safe use as a runway areanalyzed. It was found that the impact of the shock pulse load producesthe deflection with magnitude no greater than that produced when thedecelerating load passes through the critical speed.
机译:本文介绍了由冰层和冰层共同作用引起的冰盖变形 冲击载荷的作用以及随后的减速运动 在飞机降落期间加载。冲击载荷的影响和 冰盖的厚度对安全用作跑道的可能性有影响 分析。发现冲击脉冲负载的冲击会产生 变形量不大于当 减速负载通过临界速度。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号