您要查找的是不是：
- subsonic ejector 亚音速引射器
- I have no idea what subsonic speed is. 我实在不明白什么是亚声速。
- Coverplate on top side ejector plates ? 在顶出板的上面有盖板吗？
- Supersonic aircraft will not make all subsonic aircraft obsolete. 超音速飞机不会使所有亚音速飞机都淘汰。
- Figure 10-8: Ejector seat levers have catastrophic results. 图10-8 弹射操纵杆具有灾难般的后果。
- Some frame-type ejector grid designs are illustrated in Figure 3.5. 几种框架型顶料格架设计如图3.;5所示。
- Vacuum is generated by a multi-stage “Venturi” type ejector. 真空有文丘里真空发生器产生。
- Nonlinear Aeroelastic Analysis of Complete Aircraft in Subsonic Flow. 亚音速流中全飞机的非线性气动弹性力学分析。
- Some suction is provided by the ejector scrubber and the tail gas fan. 喷射洗涤器和尾气排风机可提供部分吸力。
- Can we add ejector sleeves or ejector pins in the boss of this part? 产品的这个位置不能出模，我们打算做行位，在此面上会有分模线，你接受吗?
- Some suction is provided by the ejector scrubber and the tail gas fan . 喷射洗涤器和尾气排风机可提供部分吸力。
- The float localizer presses the rubber and works as the ejector,so it ... 采用浮动定位块使橡胶压缩成形,同时作出件器,简化了模具结构。
- This airplane can go out to high subsonic speeds very easily without using afterburner. 这架飞机能够很轻松地在不打开加力的状态下飞到高亚音速。
- This paper presents a ALGOL program for Calculating The lift distribution on wings with control surface in steady and unsteady subsonic flow. 本文提供了计算亚音速偏转操纵面机翼的定常和非定常升力分布的算法语言程序。
- When the Switchblade returns to subsonic speeds, the wing will rotate back to perpendicular. 当这种“转向翼飞机”恢复亚音速飞行时，机翼就转回垂于直机身的角度。
- Under subsonic blowing condition,low lance position, high top and bottom blowing rate can decrease the mixing time. 在亚音速喷吹条件下降低枪位、增加顶底吹气体流量可降低均混时间;
- Just as a jet fighter needs an ejector seat lever, complex desktop applications need configuration facilities. 就像一架喷气战机需要一个弹射座椅操作杆一样，复杂的桌面程序需要设置设施。
- The empty weight to total weight ratio of subsonic maneuverable missile was given experimentally. 利用经验的预测方法对亚声速飞航导弹的空重比进行预测。
- What he envisions is an ellipsoid with tiny wings that he says can take off vertically and move like an alien spaceship, albeit at subsonic speed. 他所设想是极有椭翅膀起飞;他说像一个垂直和举措外国人飞船;不过亚音速速度.
- The results have an important reference value for selecting primary nozzle types of exhaust ejector systems. 试验结果对排气引射系统主喷管选型设计有重要的参考价值。
