接触孔（19） 的平面形状为椭圆形。
意味着它容易弯曲并恢复到初始平面形状。
Meaning it bends easily and returns to its original flat shape.
可编程切割直线和圆弧的任意平面形状零件。
平面形状排列是无法评估飞行，直到图像变得可用。
Planform alignment is impossible to assess until in flight imagery becomes available.
该项目平面形状能从主楼和巴登公共浴室中找到影子。
The plane shape is found in the main building and also in the bathhouse in Saltsjöbaden.
确定平面形状控制参数，并进行极限值的检查修正。
The control parameters can be got and the results should be checked and be corrected if over limit.
白色大理石柜台和壁炉反映了建筑灰泥包装的平面形状。
White marble counters and hearth reflect the planar forms of the building's stucco wrapper.
试验表明，展宽纵轧是简单易行的中板平面形状控制的有效方法。
The test shows that this technology is simple and easy to operate and is an effective measure for the shape control of the plate.
利用弹性力学的空间分析方法分析了采场平面形状与水平构造应力之间的关系。
Based on the spatial analysis method of elasticity mechanics, the relation between the shape of the plane stope and horizontal construction stress was analysed.
该方法可方便地用于非均匀布桩、非规则平面形状桩筏基础的计算和优化分析。
In addition, the analysis of the piled raft foundation with irregular shape of raft and the optimization of pile-layout could be easily carried out.
采用显式动力学有限元软件来模拟中厚板轧制成形过程中的平面形状控制问题。
Simulation of the plate rolling was performed using the dynamic explicit finite element software.
该方法适用于任意平面形状的高层建筑筒体结构及剪力墙结构的稳定及二阶位移分析。
This paper combines the column shell curvilinear strip with the slab plate strip to analyse the overall stability and second-order displacement of tall tubular structures.
其平面形状是梯形的，并且建筑最大化的利用了基地的可使用面积，这也是客户的要求。
The plot is trapezoidal, and the building adapts to it using the maximum surface area allowed, as it was required by the client.
此外，下面的表格，而不是直接在皮肤减少现有的房子，以简化的几何形状，平面形状。
In addition, rather than following the form directly, the skin reduces the geometries of the existing house to simplified, planar shapes.
从平面形状、剖面形状、发育高度及中心轴变化方面，总结了华北煤田陷落柱的几何特征。
The geometrical characteristics of sunken column in North China Coalfield is summarized from the aspects of its planar shape, sectional shape, development height and axle center change, etc.
通过某机双三角机翼平面形状的优选，表明系统具有较高的实用性，并与工程实践相吻合。
Optimization for the double delta wing platform of a new advanced trainer shows that the system is quite applicable and the results …
通过某机双三角机翼平面形状的优选，表明系统具有较高的实用性，并与工程实践相吻合。
Optimization for the double delta wing platform of a new advanced trainer shows that the system is quite applicable and the results are in good...
通过某机双三角机翼平面形状的优选，表明系统具有较高的实用性，并与工程实践相吻合。
Optimization for the double delta wing platform of a new advanced trainer shows that the system is quite applicable and the results are in good agreement with the engineering practice.
试验中进行了扑动频率、风速、迎角、机翼平面形状、翼型弯度对机翼气动特性影响的研究。
The effects of flapping frequency, wind velocity, Angle of attack, plane shape of wing and cambered aerofoil are investigated.
系统还包括平面形状控制、动态规程自动设定和控制轧制技术，构成一个较完善的控制系统。
Plan view control, dynamic regulation automatic setting system and controlled rolling technology are also included in this system.
因此研究中厚板轧制平面形状控制对提高中厚板轧制的成材率和产品质量及节能降耗至关重要。
So it is significant to study the plan view pattern control technique for improving plate yield and plate quality and to save conserve energy.
介绍了中厚板轧制平面形状的变化规律 ，阐述了勿需切边生产方法的原理、实施步骤及软件的开发。
This paper introduces the variation of plan view during plate rolling, the principle and procedure of trimming-free plate production.
考虑的目标有成本、与良好邻里环境影响地段和不良邻里环境影响地段的接近程度以及开发用地的平面形状等。
The considering objectives in the model are cost, proximity with desirable and undesirable neighboured environment effected sector of an area and the plane shape of the land for development.
文中运用该方法对十个不同平面形状的机翼进行了二十九种状态的颤振计算，并和风洞颤振实验结果作了比较。
This method was applied to flutter calculations of 29 cases for wings with 10 different types of plan forms.
在数值计算的基础上，提出了后浇带的留置间距、封闭时间的理论值，并对后浇带的平面形状提出应注意的问题。
The theory value of the spacing and the time sealing of the later joint-filled slots and some proposals on the plane form are presented on the basis of numerical calculation.
通过对等效照明面积的分析，给出了能计算任意平面形状、有遮挡效应的二面角反射器后向雷达散射截面的工程方法。
Through the analysis of EIA, a modified computational method is given, which can analyze a dihedral corner reflector with arbitrary shape of planes and with shadow objects.
在平面形状优化基础上，在机翼容积不变约束下，再采用剖面翼型优化设计，通过机翼剖面细微变化弱化较大马赫数下的激波、减小激波阻力。
In the second design step, improvement of wing's aerodynamic characteristic is mainly depended on the weakening of shock which reduces wave drag during the wing section optimization.
在平面形状优化基础上，在机翼容积不变约束下，再采用剖面翼型优化设计，通过机翼剖面细微变化弱化较大马赫数下的激波、减小激波阻力。
In the second design step, improvement of wing's aerodynamic characteristic is mainly depended on the weakening of shock which reduces wave drag during the wing section optimization.
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