dnf女漫游鹰枪3连:翻译下面文章

原文
Spinal injury in a U.S. Army light observation helicopter.
All accident reports involving U.S. Army OH-58 series helicopters were analyzed to determine vertical and horizontal velocity change at impact and the relationship of this kinematic data to the production of spinal injury. This analysis determined that spinal injury is related primarily to vertical velocity change at impact and is relatively independent of horizontal velocity change. The dramatic increase in the rate of spinal injury occurring just above the design sink speed of the aircraft landing gear (3.7 m/s) suggests that the fuselage and seat provide little additional impact attenuation capability above that of the gear alone. It is concluded that if this aircraft were modified to provide protection to the occupants for impacts up to 9.1 m/s (30 ft/s), approximately 80% of all spinal injury incurred in survivable accidents could be substantially mitigated. The incorporation of energy absorbing seats is recommended.

翻译文
在一个美国籍的陆军的针的受伤点燃船搬运观察直升飞机。
包括美国陆军哦 -58 系列直升飞机的所有意外事件报告被分析决定垂直的和在冲击和针受伤的生产的这运动学的数据的关系水平的速度变化。 这一项分析决定了针的受伤在冲击被主要地讲到垂直的速度变化和不受水平速度变化的控制是相对地。发生仅仅高于设计的针受伤的比率的戏剧性的增加滑落飞机起落架 (3.7 m/s) 的速度建议机身和位子提供在独自地的齿轮上面的小另外的冲击变薄能力。 一般得出结论，如果这一架飞机被修正为达 9.1 m/s(30 ft/s) 的冲击提供保护给占有者,在 survivable 意外事件被招致的大约 80% 所有的针受伤可能是实质上镇静。 吸收位子的能源的结合被推荐。