1)  statically indeterminate truss
静不定桁架
1.
Based on the traditional method of making geometrical chart,the analytical expressions of deformation compatibility equation of statically indeterminate truss is obtained in this paper.
:在传统的几何作图法的基础上,导出了静不定桁架变形协调方程的解析表达式。
2)  statically indeterminate
静不定
1.
That is, do it by means of the thoughts in solving statically indeterminate problems.
建议采用解静不定问题的力学思想导出圆轴扭转剪应力公式,从而加强学科思想的教学。
2.
In this paper, the stability of compressive rod and structure (statically indeterminate structure) is analyzed.
结构的承载能力包括强度、刚度、稳定性,本文对含有压杆的结构(含静不定结构)进行了稳定性的分析,对结构的临界载荷与结构失稳的最小载荷进行了研究,对压杆的临界载荷公式进行了分析。
3)  statically indeterminate shaft
静不定轴
1.
By using the boundary conditions of the statically indeterminate shaft with three fulcrums,the deflection curve square of the shaft is got;By utilizing the energy method to improve the calculation formula, the accurate first order critical speed of the statically indeterminate shaft with three fulcrums is obtained quickly.
通过满足三支点静不定轴的边界条件来求解基本方程,得到多跨静不定轴的挠曲线方程,并应用能量法改进了计算公式,快速准确地求得三支点静不定轴的一阶临界转速。
4)  static instability
静不稳定
1.
Compared with general aeroplane,tailless aeroplane has static instability in longitudinal mode.
通过对无尾飞机与常规布局飞机进行比较,针对其纵向静不稳定采用增稳系统的纵向控制律设计方案,增稳系统用法向加速度反馈信号为主反馈,并设计纵向控制律。
2.
With introducing the ACT to overall design of an Air to Air Missile(AAM), this thesis analyses the capability improving of the AAM because of using the RRS design, and sets forward the stability criteria for static instability missile body.
讨论了放宽静稳定性设计对导弹性能的改善 ,最后给出了静不稳定弹体的系统稳定性判定条件 ,并着重讨论了静不稳定弹体的人工稳定问题。
3.
The active control technology(ACT) which had been used widely in the field of plane design is introduced to overall design of air to air missiles, and the judge criterion of stability for static instability missile body is brought forward.
将飞机设计领域广泛采用的主动控制技术引入空空导弹的总体设计中,提出了空空导弹放宽静稳定性设计问题,给出了静不稳定弹体的系统稳定性判定条件。
5)  statically determinate(indeterminate)
静(不)定
6)  static unsteady
静不稳定
1.
After a thorough investigation of the bifurcation behaviors of the nonlinear model of an inherently static unsteady aircraft at high angles of attack,eigenstructure assignment was applied to design the longitudinal control law and gain scheduled lateral control law.
在充分了解本体静不稳定飞机大迎角非线性数学模型的分叉特性的基础上 ,以分叉分析方法作为指导 ,采用特征结构配置方法设计纵向控制律和调参的横航向控制律。
2.
Bifurcation Analysis and Catastrophe Theory Method (BACTM) was applied to a nonlinear dynamics model of an inherently static unsteady aircraft to calculate the equilibrium curve while regular control surfaces deflected.
针对某静不稳定飞机的非线性动力学模型 ,采用分叉与突变理论 (BACTM)计算了常规控制面变化的飞机本体平衡曲线 ,揭示了其固有的在大迎角下的开环运动特性。
参考词条
补充资料:不定
【不定】
心所名。所谓不定,是说这四种法,可以成就善,也可以成就恶,故曰不定。
  一、悔,悔者追悔,也就是事后生悔,如作了善事而后悔则属恶,作了恶事而后悔则属善,故列入不定;
  二、眠,即睡眠,若睡眠是为了调摄身心,恢复体力,便是善,若为了贪睡,或昼夜颠倒,耽误正业,便是恶;
  三、寻,寻者寻求事理,若想善便是善,若想恶便是恶;
  四、伺,寻是粗想,伺是细想,伺察事理叫做伺,若细想为善便是善,细想为恶便是恶。
说明:补充资料仅用于学习参考,请勿用于其它任何用途。