机翼前缘肋 nose ribs
前缘翼肋
Leading edge fin
以上为机器翻译结果，长、整句建议使用 人工翻译 。
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.
youdao
应用推荐
模块上移
模块下移
不移动