| 1. | Quantitative flow visualization on unsteady flow fields of wing rock
滚摆非定常流场的定量流动显示 |
| 2. | Numerical simulation of unsteady flows induced by an accelerating projectile
加速弹丸诱导的非定常流场数值模拟 |
| 3. | Numerical simulation of three - dimensional steady flow field with varing specific heat in a two - stage turbine
某型两级涡轮变比热容三维定常流场的数值模拟 |
| 4. | Numerical simulation of the unsteady flow in a transonic turbine stage is still a hard work for cfd researcher
涡轮级内的非定常流场数值模拟是现阶段计算流体力学研究的重要领域，也是研究的难点。 |
| 5. | A high accuracy , high resolution numerical method ( lu - sgs - ge scheme and 4th order muscl tvd scheme ) is applied to calculate the unsteady flow field
在计算网格移动下的非定常流场时采用了高精度、高分辨率的数值计算方法? ? lu - sgs - ge隐式格式和高阶muscltvd格式。 |
| 6. | Basing on the static aeroelasticity , the jig - shape and the attack angle design have been studied . generally , much computing time is needed in unsteady flow computation
利用现有条件自主开发出适合定常、非定常流场计算和气动弹性研究的分布式并行计算机系统。 |
| 7. | In two - dimensional electrokinetic focusing , a theoretical model based on kirchhoff s current law was derived and applied to predict the width of the electrokinetically focused stream
在三维定常流场混合问题方面，我们以数值模拟方式探讨电渗流在具异质性表面电荷分布之三维微管道中之混合，共有三种不同型态之混合管道被探讨。 |
| 8. | The results of solving the unsteady flow fields that are in agreement with the experiments show that the unsteady flow field solver is correct and the unstructured dynamic mesh technique of the dissertation is well robust
非定常流场的计算结果与实验结果符合的很好说明本文非定常流场计算正确，非结构运动网格可靠、鲁棒性好。 |
| 9. | Furthermore , numerical simulations for steady or unsteady transonic flow of rae2822 and dfvlr - r2 supercritical airfoils and a supercritical wings are investigated . the numerical results are in good agreement with experimental data where available
进而，应用该解算器对超临界翼型rae2822 、 dfvlr - r2及某超临界机翼的定常或非定常流场进行了数值计算研究，得出了良好、合理的结论。 |
| 10. | The unsteady flow as thrust vectoring nozzle deflecting dynamically is investigated . the method of calculating the unsteady flow in the nozzle is given and the flow of the nozzle in the maximum power setting and maximum a / b power setting of the engine is calculated
研究了矢量喷管动态偏转过程中气流的非定常流动和矢量喷管非定常流动计算方法，计算了矢量喷管在发动机某中间状态和加力状态下的非定常流场。 |
