2) static aeroelasticity
静气动弹性
1.
Realizing data exchange to reflect coupling between fluid and structures is essential to solving static aeroelasticity problems.
研究静气动弹性问题一大关键是要解决流固数据耦合。
2.
Three force equilibrium methods of static aeroelasticity are compared with.
介绍了惯性释放理论以及基于CFD/CSD耦合的静气动弹性计算方法,比较了静气动弹性计算中的三种系统载荷平衡方法。
3) static aeroelastics
静气动弹性
1.
In order to eliminate the influence of static aeroelastics deformation and satisfy the flying characteristic requirement of aircraft, a new approach to the jig-shape elastic wing design problem is presented.
采用三维N-S方程为控制方程,计算机翼所受的气动力与静气动弹性平衡方程耦合求解。
2.
On this base, the static aeroelastics problems of wing and aircraft are investigated by coupled with structure dynamic equation.
本文的主要工作是利用计算流体力学(CFD)方法,对三维机翼以及全机的定常流场进行了数值模拟;并在此基础上耦合结构力学方程研究了三维机翼以及全机的静气动弹性问题。
4) static aeroelastic
静气动弹性
1.
In the study,the aerodynamic analysis of wing is achieved by solving 3D unstructured Euler equations,which integrated static aeroelastic effect.
采用三维Euler方程为控制方程,耦合静气动弹性平衡方程,进行机翼静气动弹性数值模拟;在机翼静气动弹性分析的基础上,结合Takanashi余量修正方法对三维大展弦比机翼进行气动外形反设计,以确定机翼的型架外形。
2.
As a function of flight dynamic pressure, angle of attack, deflection of horizontal tail and longitudinal acceleration, the longitudinal static aeroelastic response characteristics of an aircraft are analyzed by using two static aeroelastic analysis methods, i.
分别使用线性和非线性静气动弹性分析方法,对某飞机纵向静气动弹性响应特性随飞行动压、攻角、平尾偏度和纵向过载变化的趋势进行了分析,并将分析结果和飞行试验进行了比较。
6) air trajectory under no wind
静止空气弹道
补充资料：平心静气
1.亦作"平心定气"。亦作"平心易气"。 2.心情平和，态度冷静。
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