nose ribs
... 前缘肋 nose rib 前缘效应 leading edge effect 强制开伞拉绳 static line ...
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机翼前缘肋 nose ribs
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使用有限体积法计算了飞行时的气动载荷，分析了前缘切口和翼肋开孔对压强分布的影响；
The finite volume method was used to compute the aerodynamic load, and the effect of leading-edge cut and ribs on the pressure distribution was analyzed simultaneously.
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