| 1. | By comparion , the value of calculation is good to worth with actual measurement
通过比较计算值与实测值吻合良好。 |
| 2. | The calculating result and the experiment result was compared to supply the reliable curve
同时，比较计算结果与实验结果，进行误差分析。 |
| 3. | Select the operator that you want the filter to use to compare the evaluated field and the value
“运算符”中，选择希望筛选器用来比较计算字段和值的运算符。 |
| 4. | The program is easy to be mastered and the calculating speed is fast . the precision of the program is pleased compared with the model test
以上程序数据处理灵活、易于调用、便于掌握、计算速度快，与实测值比较计算精度高。 |
| 5. | By analysis and comparison of the results , we draw the conclusion as follows : firstly , the quantum tunneling effect is quite pronounced
通过分析和比较计算结果，我们得到如下结论。第一，体系的能量-反应几率变化曲线说明量子隧道效应显著。 |
| 6. | The one is person is still regarded as rational one , whose main behavior terms is comparison between earn and cost , and pursuit of maxim of benefit
一是制度变迁中的人仍然看作理性经济人,其最主要的行为特征就是收益与成本的比较计算,并追求利益最大化。 |
| 7. | Put the wind load on the modal , results will be obtained , compared with results in test , we are assured that the outcome is dependable
将已经得到的时域风载加在模型上,计算得到时域中各种风振响应结果。比较计算结果与实验结果,可以发现计算与实验是相符的。 |
| 8. | The paper researches the vortex moment caused by the shape and locality error of one hole in the sphere socket . by analyzing and comparing the result we can find the method to decrease the vortex moment
本课题只研究球窝其中的一个节流孔的形状和位置误差所引起的涡流力矩,通过分析比较计算结果,从而找到减小涡流力矩的方法。 |
| 9. | 2 to meet the need of aerodynamic configuration optimization design in supersonic state , different supersonic drag prediction methods have been compared and the supersonic performance calculation method suitable for optimization design system has been obtained
为适应超音速气动外形优化设计要求，对不同的超音速阻力计算方法进行了比较计算和分析，建立了与优化设计相适应的超音速气动特性计算方法。 |
| 10. | At last this paper also analyses special - shaped section columns subjected to biaxially eccentric loading using finite element program ansys5 . 7 . according to comparing of analytical results , the ductile behavior of r . c . t , l - shaped and " + " shaped columns are investigated
本论文最后采用大型有限元程序州sys5 . 7对上述几种截面柱构件也进行了分析，通过比较计算结果，得出异形截面柱延性变化规律，并检验本论文所编制分析程序的可靠度。 |
