摘要: An experimental program was conducted to evaluate a landing gear concept that redistributes the impact energy of an autorotational landing. This landing gear concept redistributes the impact energy by providing an interconnection ... 展开
作者 | logan, a. h. waldon, c. a. | ||
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原报告号 | ADA065298 | 总页数 | 120 |
主办者 | Non Paid ADAS | ||
报告分类号 | [51C - Aircraft, 51B - Aeronautics] | ||
报告类别/文献类型 | AD / NTIS科技报告 | ||
关键词 | Landing gear Helicopters Aircraft landings Energy absorbers Impact shock Helicopter rotors Autorotation Nose wheels Pitch(Motion) Drop tests Hydraulic equipment Impact strength OH-6A Helicopters H-6 Helicopers |