1.
Numerical Simulation of the Low Wind Speed Flow Fields around the Symmetrical Airfoil
对称翼型低速绕流流场特性的数值分析研究
2.
THE ASYMMETRIC DISCARDING SABOT MODULE OF APFSDS
尾翼稳定脱壳穿甲弹卡瓣膛外非对称脱壳模型
3.
In the method, such an airfoil is termed a four-segment airfoil.
在方法,这种称为翼型四个部分机翼.
4.
The two wings of the building are exactly symmetrical.
大楼的两翼完全对称。
5.
"All species are less than 18 in. (45 cm) long and have winglike, rigid fins and an unevenly forked tail."
体型皆小,最大约长45公分,具翼状硬鳍和不对称的叉状尾部。
6.
The Investigation of the Effect of Airfoil Modification on the Aerodynamic Performance of Supercritical Airfoil
翼型改型对超临界翼型气动性能影响的研究
7.
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
8.
Airfoil design of a micro-flapping wing based on CFD
基于CFD方法对微型扑翼翼型设计的研究
9.
An airfoil whose principal function is providing lift, especially either of two such airfoils symmetrically positioned on each side of the fuselage of an aircraft.
机翼主要功能是提供升降的机翼，尤指飞机机身两侧对称位置上的
10.
Fix the wings on the fuselage with screws, check if they are symmetry for fuselage.
将机翼用螺钉固定在机身上，检查机翼是否对称于机身。
11.
The effects of wind-tunnel model design on flowfield and aerodynamic behavior for large aspect-ratio wings
大展弦比机翼模型设计对翼型流场气动特性的影响
12.
Effect of Aerofoil Camber on Airfoil Aerodynamic Performance
风力机的翼型弯度对风力机翼型气动性能的影响
13.
A variant of the swept-back wing is the delta wing.
后掠翼的变型是三角翼。
14.
(2)Symmetrische Formbesass 23±4.20%,asymmetrische Form besass 77±4.20%. 3.Typenform der A. cerebri ant.
(2)对称型23±4.20%,不对称型77±4.20。
15.
The Initial Exploration How the Coming Flow and Wing Flapping Mode Influence the Aerodynamic Parameters of Micro Aerial Vehicles;
来流及翼扑动方式对微型扑翼飞行器气动参数影响的初探
16.
Conclusion Alar cartilaginous fibrous ring and alar cartilaginous mus- cular ring are very important anatomic structures to maintain the shape of the lower part of the nose.
结论鼻翼软骨纤维环和鼻翼软骨肌肉环是维持外鼻下端形态和鼻孔对称的重要解剖结构。
17.
THE EFFECTS OF WIND-TUNNEL MODEL VIBRATION ON FLOW FIELD AND AERODYNAMICS OF AN AIRFOIL
模型振动对翼型流场和气动性能的影响
18.
Numerical Analysis on a Two-degree-of-freedom Self-excited Airfoil with Asymmetry Freeplay Model;
具有不对称间隙的二元机翼自激振动的数值分析