1) jet driving rotor
翼尖喷流
1.
To implement the jet driving rotor which jets at the rotor-tip,the flows inside the conductive pipe were numerically simulated,and the effect of the flows inside the conductive pipe by outlet shape was analyzed.
数值模拟计算了为实现旋翼翼尖喷流驱动的引流管道内部流动,分析了管道出口形状对引流管道流动的影响。
2) tip dragger; wingtip
翼尖扰流片
3) wingtip assembly
翼尖整流罩
4) rotor-tip burner
旋翼桨尖喷嘴
6) winglet
[英]['wiŋlit] [美]['wɪŋlɪt]
翼尖小翼
1.
To match these needs,a bigger wing aspect ratio and winglet are adopted as the improvement measures,hopefully the lift-drag ratio of the modified UAV could be increased.
为延长某无人机的留空时间,加大航程和提高升限,用适当加大机翼展弦比和加装翼尖小翼的办法对原型机的气动特性进行了改进,以期能使该无人机的升阻比有较大提高。
2.
Modification of winglet is adopted to raise the lift-drag ratio of the UAV for extension endurance,for enlarge range and for increase ceiling.
为延长无人机留空时间,加大航程和提高升限,可采用加装翼尖小翼的方法使无人机的升阻比有所提高。
补充资料:Al-Li合金构件——歼7-II飞机舱口盖及副翼扰流片
Al-Li合金构件——歼7-II飞机舱口盖及副翼扰流片
Al—Ll合金构件——歼7一I 1机舱口盖及副翼扰流片 张自供稿
说明:补充资料仅用于学习参考,请勿用于其它任何用途。
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