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1)  missile stability
导弹稳定性
2)  elastic stability
弹性稳定
1.
By using elastic stability theory and in combination with field work,a method in calculating space when installing sucker rod lifter is worked out and an example is provided.
运用纵横弯曲梁及弹性稳定理论,结合工程实际,分析得出了在全井各种井段合理安装抽油杆柱扶正器间距的计算方法,并给出了计算实例。
2.
And a quantitative approach is also provided to determine the elastic stability and survival ability of the single-pile wellhead while the future wellhead retention operation above the seawater is goi.
根据生产实践中常遇到需要在海面以上保留井口的问题,在不考虑水平荷载作用的前提下,从弹性稳定性研究方法入手,采用能量法研究单桩井口在轴向集中荷载和均布荷载条件下的弹性稳定性,为今后海上保留井口作业时,校核单桩井口弹性稳定性及生存能力,提供一种定量计算方法和分析的依据。
3.
Based on the principle of energy,the paper discusses the elastic stability of high pier with non-uniform section.
本文基于功能原理,讨论了变截面桥墩的弹性稳定性。
3)  unstable missile
不稳定导弹
1.
It has been concluded that the inner loop of a three-loop autopilot is an attitude autopilot,it can make an unstable missile stable;missile aerodynamic coefficient change and fin control surface bias do not have effects on the steady state outputs of three-loop autopilots.
研究表明,这种驾驶仪的内回路是姿态驾驶仪,可以对静不稳定导弹进行稳定,闭环稳态传递系数不受气动参数变化的影响,驾驶仪输出对舵机零位误差不敏感,系统响应速度较带积分校正的过载驾驶仪快,且三回路驾驶仪比标准驾驶仪对噪声有较强的滤波能力。
4)  elastic stability
弹性稳定性
1.
Study on the elastic stability of bottom holes assembly with controllable eccentric stabilizer and its application;
可控偏心稳定器钻具组合弹性稳定性研究及其应用
2.
Study on critical load and elastic stability of drilling riser;
钻井隔水导管临界载荷及弹性稳定性研究
3.
Elastic stability of open end cylindrical shell arising from shell hydroformng is studied by the nonlinear elastic stability theory.
利用非线性弹性稳定性理论 ,分析研究了壳体液力成形工艺中的开口圆柱壳弹性稳定性问题。
5)  projectile stability
弹丸稳定性
6)  aeroelastic stability
气弹稳定性
1.
Modeling study on tilt-rotor's aeroelastic stability in cruise flight
前飞状态倾转旋翼机气弹稳定性建模
2.
The multi-body analysis of the aeroelastic stability of the tiltrotor aircraft is presented.
以半展长弹性机翼全铰接式倾转旋翼机模型为例,在直升机模式下分析了桨叶摆振刚度及飞行速度对倾转旋翼机气弹稳定性的影响。
3.
This paper addresses the developed structural modeling and aerodynamic modeling of aeroelastic stability analysis software for rotor blade with new tip.
本文介绍了所开发的新型桨尖的气弹稳定性分析软件的结构模型、气动模型特点,采用ITR旋翼进行了算例验证,并用25B1。
补充资料:连续性与非连续性(见间断性与不间断性)


连续性与非连续性(见间断性与不间断性)
continuity and discontinuity

11an父ux泊g四f“山。麻以角g、.连续性与非连续性(c。nt,n琳t:nuity一)_见间断性与不间断性。and diseo红ti-
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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