摘要: A design study has been conducted to define a landing gear concept that redistributes the impact energy of an autorotational landing in a manner that minimizes the occurrence of blade/tailboom strikes. The landing gear concept red... 展开
作者 | logan, a. h. | ||
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原报告号 | ADA029372 | 总页数 | 88 |
报告类别/文献类型 | AD / NTIS科技报告 | ||
关键词 | Landing gear Helicopters Skids Rotor blades(Rotary wings) Pitch(Motion) Life cycle costs Cost analysis Roll stress analysis Energy absorbers Weight Resonance Helicopter rotors OH-6A Aircraft H-6 Aircraft Tailboom interference Design Autorotation |