1.
Design methods of steel-concrete composite beams with opening in concrete flange and its engineering application
混凝土翼缘开洞的钢-混凝土组合梁设计方法及工程应用
2.
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
3.
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
4.
During fabrication slots for the stringers flanges were flame cut into box girders.
制造时，为安装纵梁翼缘，在箱型梁中用焰割法开槽口。
5.
The behavior and performance of the cracked flange plates suggest that good levels of fracture toughness exist in the A 517 steel.
开裂的翼缘板的性能及使用状态说明A517钢的断裂韧性良好。
6.
leading-edge flap position indicator
前缘襟翼位置指示器
7.
trailing-edge flap position indicator
后缘襟翼位置指示器
8.
The ailerons are movable sections along the rear edges of the wings.
副翼是机翼后缘的可动部分。
9.
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.
10.
The Relation of Closing up and Separating between the New Feeling Writer and the Left Wing Literary Arena;
新感觉派作家与左翼文坛的缘起缘落
11.
with out spread arms [wings] = with arms [wings] outspre ad
以张开的双臂 [翼]
12.
The slab has provided greater fixity to the top flange, and the adjacent web gap has experienced greater deformation and has cracked first.
桥石板为上翼缘提供了很大的固结度，于是相邻的腹板间隙就经受了较大的变形并且首先开裂。
13.
There are two methods for welding radial stiffeners to bias-rail box girder: welded all around and open at tensile flange.
起重机偏轨箱形梁横向加强板有加强板四周均焊和在受拉翼缘处空开2种焊接方式。
14.
A seagull hit the right wing tip, leading edge flap sustained minor damage.
右翼尖与一只海鸥相撞，前缘襟翼受到轻微损伤。
15.
Wind Tunnel Experiments of Symmetric Discarding Sabot Disturbance of APFSDS Projectile
尾翼脱壳穿甲弹对称脱壳的风洞实验
16.
A Numerical Wind Tunnel Study on Distance between Tail Wing and Rear Hood and Angle of Attack of Tail Wing of a Car Model Using CFD;
轿车尾翼间隙和攻角的数值风洞研究
17.
Wind Tunnel Investigation on Dynamic behavior of 80°/65° Double Delta Wing in Rolling at High Incidence
80°/65°双三角翼摇滚特性风洞实验研究
18.
The effects of trailing edge jets on the vortex breakdown location over a delta wing
三角翼后缘喷流对前缘涡破裂位置的影响