Helicopter External Sling System Basic Vibration Data

机译：直升机外部吊索系统基本振动数据

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Simulated tests were conducted of helicopter externally slung loads ranging from 2,000 to 4,000 pounds on an analog computer. (Author)

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Cottingham, G. M.;
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年度 1969
页码 p.1-11
总页数 11
原文格式 PDF
正文语种 eng
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关键词
Cargo ; Helicopters ; Airborne ; Suspension devices ; Fastenings ; Loading(Mechanics) ; Shock(Mechanics) ; Vibration ; Resonance ; Programming(Computers) ; Simulation;

机译：货物;直升机;空降;悬架装置;紧固件;装载（机械）;冲击（机械）;振动;共振;编程（计算机）;模拟;

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Helicopter External Sling System Basic Vibration Data

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