1) tip acceleration
翼尖加速度
1.
The test method include root bending moment measurement and tip acceleration measurement.
通过实验检验了实验方案的正确性、可行性,并通过垂尾的根部弯矩测量和翼尖加速度测量得到了双垂尾的抖振响应曲线和抖振起始迎角,掌握了边条翼布局的双垂尾抖振响应随迎角变化的规律,即在抖振起始迎角之前,双垂尾的抖振响应很小且基本不随迎角变化,当迎角超过抖振起始迎角时,抖振响应急剧增加并在某一迎角范围达到最大值,之后抖振响应逐渐降低。
2) tip speed
翼尖线速度
3) wingtip stalling
翼尖失速
1.
Characteristics of tailless aircraft wingtip stalling, including common and unique characteristics compared with other configurations, are analyzed with emphasis placed on the effect of wingtip stalling on flying qualities of tailless aircraft.
首先分析了无尾飞机翼尖失速的特点 ,包括与其他布局形式共有的和自身特有的特点 ,重点是翼尖失速对无尾飞机飞行品质的影响。
4) accelerating cascade
加速翼栅
5) Tip Velocity
尖端速度
1.
The results indicate that,with increase in undercooling,a small nuclei will grow developed dendritic,the tip velocity at steady state is become faster;With increase in the coupling parameter,tip velocity at steady state increased monotonically and it's interfacial stabil.
结果表明,随着过冷度值的增加,晶核由一圆核逐渐发展为发达的枝晶,相应的枝晶稳态尖端速度明显加快;随着耦合系数的增大,晶核由一圆核发展为细长的枝晶,枝晶的稳态尖端速度呈单调递增趋势,界面的稳定性逐渐变差。
6) fip speed
桨尖速度
补充资料：变后掠翼飞机(见后掠翼飞机)
变后掠翼飞机(见后掠翼飞机)
swing-wing aircraft
bianhoul位eyi feiii变后掠翼飞机(swing一wing aircran)见后掠翼飞机。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条