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wing section

基本解释翼截面

网络释义

1)wing section,翼截面2)aerofoil section,翼型截面3)aerofoil section,机翼型截面4)T-shaped sectional flange,T型截面翼缘5)flange-closed sections,翼缘闭合截面6)airfoil-section funnel,翼型截面烟囱

用法和例句

Based on the hollow flange beam(HFB) of Australia,the two new kinds of cold-formed flange-closed sections are put forward in the paper.

目的分析提出的两种新型(HF1、HF2)冷弯翼缘闭合截面在轴压荷载作用下的力学性能。

Fast Approximate Analytical Method of Wing Cross-section Distributed Loading

翼截面分布载荷及节点分配的快速近似方法

Elastic buckling of web restrained by flanges in I-section members

考虑翼缘约束的工字形截面腹板的弹性屈曲

Rectification of computation method for section efficiency index of T beam with wet joint in web plate

翼板湿接T梁截面效率指标计算方法修正

RESEARCH ON LOCAL BUCKLING OF LIPPED H-SECTION MEMBERS

卷边翼缘工形截面构件的局部稳定性能

LATERAL STABILITY BEHAVIOR OF LIPPED H-SECTION BEAMS SUBJECTED TO MOMENTS

卷边翼缘工形截面梁的稳定性能及设计方法

Experimental Investigation on Flow Field Around Blade-tip Airfoil Section of Horizontal-axis Wind Turbine

水平轴风力机叶尖翼型截面流场的试验研究

Abstract: A model of self-excited ae rodynamic forces acting on a sectionof bridge deck with additional surface atta ched below the trailing edge is established.

文摘:首先建立了下风侧附加翼板桥梁主梁截面的自激气动力模型。

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

LOAD-CARRYING CAPACITY OF LIPPED H-SECTION MEMBERS UNDER AXIAL LOAD

卷边翼缘工形截面构件在轴心压力作用下的稳定承载力研究

THE EFFECTIVE FLANGE WIDTH OF BEAM SUPPORT SECTIONS IN CAST-IN-SITU FLOORS UNDER VERTICAL LOADS

竖向荷载下现浇楼盖中的梁支座截面有效翼缘宽度

Experimental Research and Analysis of Effective Flange Width of Beam End Section in Cast-in-Situ Concrete Frames

现浇混凝土框架梁端截面有效翼缘宽度的试验研究与分析

Multiple objectives optimization of hingeless rotor tapered box-beam blades based on aeroelastic stability

无铰旋翼变截面盒型梁桨叶气弹动力学多目标优化

RESEARCH ON IN-PLANE STABILITY BEARING CAPACITY OF LIPPED H-SECTION TAPERED MEMBERS UNDER COMPRESSION AND BENDING

卷边翼缘工形变截面构件在压弯荷载作用下平面内稳定承载性能研究

The new flap keeps essentially the same profile, but with a reduced cross sectional area at its extremities.

新副翼的形状在总体上保持不变,不过在其末端的横截面积却变小了。

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。

perpendicular cut

(与轴成)垂直(截面)截割

area of blade sectio

叶片截面面积桨叶截面面积

sampling cross-section [station]

取样横截面[部位]

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