1.
ANALYSIS OF DEFECT LIMIT AND REINFORCEMENT OF THE OPENINGS ON THE FLANGE PLATE OF STEEL REINFORCED CONCRETE COLUMN
型钢混凝土柱翼缘开孔缺损率限值及补强分析
2.
These cracks occurred at either the beam flange or in the column flange depending on the reentrant corner weld angle.
这些裂纹视凹形焊角的不同，或者出现在横梁翼缘上，或者出现在立柱翼缘上。
3.
The second crack is a crack originating at the groove weld toe of the column flange-girder flange connection.
第二种是产生于立柱翼缘与主梁翼缘连接处的坡口焊缝焊趾处的裂纹。
4.
The Limit Value of Axial Compression Ratio of Reinforced Concrete Special-Shaped Columns;
T形、十字形截面柱翼缘对轴压比限值影响的讨论
5.
According to the relationship between the structural strength and slenderness of plate elements, the limited width-to-thickness ratio of the flange of a box-section column under seismic load is derived.
由构件承载力与壁板宽厚比的关系,得出了抗震设计箱形截面柱翼缘板宽厚比限值。
6.
Study on Mechanical Behavior of Top and Seat Angle Connections
上下翼缘角钢半刚性梁柱节点的力学性能研究
7.
Theory Studies on the Behaviors of Beam-Column Connections with Beam-End Horizontal Haunch;
梁端翼缘扩大型梁柱节点受力性能理论分析
8.
Experimental Evaluation on the Behaviors of Beam-To-Column Connections with Beam-End Horizontal Haunch;
梁端翼缘扩大型梁柱节点受力性能的试验研究
9.
Crack resistance of RC joints with specially shaped columns considering the effect of flange length
考虑翼缘影响的异形柱框架节点抗裂性能分析
10.
Seismic behavior and design method of beam-to-column connections with beam-end horizontal haunches
梁端翼缘扩大型梁柱节点抗震性能和设计方法
11.
Experiment on Welded Flange Plate (WFP) Reinforced Conneciion
钢结构焊接翼缘板加强式梁柱刚性连接的试验研究
12.
Research on Seismic Behavior of Steel Frames with Reduced Beam Sections;
采用翼缘削弱型梁柱节点的钢框架的抗震性能研究
13.
Study on Behavior of Extended End-plate Connection Joint with Reduce-beam Section in Beam-to-column Weak-axis Direction
翼缘削弱型外伸式端板连接节点在梁柱弱轴方向的受力性能研究
14.
The outer rear edge of the wing of a bird, containing the primary feathers.
翼尖，前翼鸟翼的外后缘，包括初生毛
15.
leading-edge flap position indicator
前缘襟翼位置指示器
16.
trailing-edge flap position indicator
后缘襟翼位置指示器
17.
The ailerons are movable sections along the rear edges of the wings.
副翼是机翼后缘的可动部分。
18.
a straight line connecting the leading and trailing edges of an airfoil.
连接机翼的前缘与后缘的直线.