| 1. | The problems of multiple contours to multiple contours and connected bifurcation are considered in this algorithm
在三角网格的基础上构造插值于网格点的复合三角b zier曲面。 |
| 2. | Based on former researcher ' s works , an algorithm for grid nodes extraction from thinned grid image is present
基于以前研究者的工作，提出了从细化网格图象中提取网格点的算法。 |
| 3. | Fig . 2 vertical structure of the grid points in the orsm : upper levels are close to the pressure coordinate while lower levels are terrain - following
图2 orsm网格点的垂直结构：上层趋向气压坐标，而下层坐标则随地形变化。 |
| 4. | Visually , the design surface is a rectangular area with an overlay of grid dots that you can use to align report items on the layout
从外观上看，设计图面是一个覆盖了一层网格点的矩形区域，您可以使用这些网格点在布局中对报表项。 |
| 5. | Experiment showed that the network with 6 nodes in each hidden layer has the best - forecast ability . the bp network was developed by training , b )
将反演得到的气象站点相对湿度资料，拓展为模式网格点的湿度资料，从而与数值预报模式相匹配。 |
| 6. | For clusters of 13 nd 25 sites with the special shape , the numerical results show that their gs are respectively 6 - fold and 8 - fold degeneracy ( while the gs of macroscopic antiferromagnet is singlet )
通过计算含有13个格点和25个格点的双组分海森堡反铁磁团簇，结果表明它们的基态分别是6重和8重态(而宏观反铁磁系统的基态是单态) 。 |
| 7. | This result is consistent with the experimentally observed features of short - life . that shows our model is reasonable . the parameters of the extended bbv model are as follows : the near neighbor interaction intension f = 0 . 75ev and the coefficient of the hubbard term u = 1 . 5ev
我们的模型参量为:近邻格点电子相互作用强度作0 . 75ev ，同一格点的电子相互作用强度卜1 . 5ev 。 |
| 8. | The other is based on contour line . the way is that first editing the contour line , then saving these heights , finally depending on linear calculating middle value , thus getting the height of every mesh point , and the 3d terrain model
另一种方法是基于等高线的方法，该方法是通过对等高线进行编辑，保存相应点的高程，再根据线性插值，得到各个网格点的高程，从而生成对应的地形模型。 |
| 9. | The propose of this project is to develop a three - dimensional , compressible navier - stokes solver for detailed study the flow inside transonic turbine and compressor ' s stator in the airplane turbomachinery
摘要本研究的目的在发展一系列飞机滑轮引擎之静子叶片的计算流体力学方法与程式，计算程式方面包括三维叶片格点的建立与黏性流程式开发及撰写等，程式发展完成后将进行一系列外形及气流条件计算模拟。 |
