2) rate of explosion
压力升高比
3) lift force
升力
1.
Experimental investigation of lift forces on deformed bubbles in bubbly flows at low and intermediate Reynolds numbers;
中低Reynolds数泡状流变形气泡升力的实验研究
2.
One modified droplet turbulent diffusion model was proposed by taking consideration of the effect of shear lift force on the droplet terminal settling velocity, meanwhile the effects of local relative slip between droplet and its carrying fluid together with the interface roughness of liquid film were considered.
在对气核中液滴运动进行详细分析的基础上,通过考虑剪切气流中液滴所受升力作用对液滴终端沉降速度的影响,首次在理论上实现了在液滴扩散特性计算中计及剪切升力的作用,同时在所建立的计算模型中还综合考虑了液滴和其携带流体间的局部滑移以及液膜表面粗糙度的影响,应用该模型对油气输送条件下液滴扩散特性计算的平均计算误差从 28。
3.
By means of the detailed analysis on the droplet movement under condition of oil/gas transport, one method taking consideration of the local interphase slip and the distribution of local shear rate is presented to calculate the local lift force over the pipe cross section.
通过对油气输送条件下液滴运动状态的分析 ,提出了考虑相间局部滑移和局部剪切速率分布的水平布置管线中液滴局部升力的计算方法。
4) lift
[英][lɪft] [美][lɪft]
升力
1.
Research on mechanism of bar lift force by using PIV system in wave field;
波浪场中利用PIV装置研究杆件升力形成机理
2.
Study on lift measurement of ship fins stabilizer at zero forward speed;
船舶零航速减摇鳍升力测量研究
5) lifting force
升力
1.
Some specific measure about reducing lifting force and yawing moment are advanced.
分析了作用于汽车上的空气动力对汽车直线行驶及横向稳定性的影响,介绍了减少汽车空气升力及横摆力矩的方法。
2.
This article assumes that the classic theory of lifting force ommits one crucial factor determining lifting force: pressure gradient.
认为经典升力理论遗漏了一个决定升力的重要因素:流体的压强梯度。
6) lift-drag ratio
升阻比
1.
The results show that the best effect of glide extended-rang is obtained with the adoption of maximum lift-drag ratio slide.
由数值分析得到采用最大升阻比的滑翔策略可获得最佳滑翔增程效果。
2.
The lift coefficient,drag coefficient and lift-drag ratio were obtained at a series of angles of attack, starting at 0°up to 16°at 2° intervals respectively.
利用XFO IL和FLUENT软件对NACA4412翼型(原型)及其多种改型的空气动力性能进行了数值模拟,分别对比计算了翼型在攻角为0°、2°、4°、6°、8°、10°、12°、14°和16°情况下的升力系数、阻力系数和升阻比,以改善其翼型性能;并在地效场中离地间隙分别为0。
3.
Several conclusions can be drawn: Firstly,the maximal lift-drag ratio Kmax=3.
计算结果表明该布局在Ma=6的时候,最大升阻比Kmax可以达到3。
补充资料:升力
又称“举力”。物体(如飞机)与空气相对运动时,作用于物体上的垂直于气流方向的力。机翼是飞机产生升力的主要部件,机身和水平尾翼也可产生部分升力。升力的大小取决于飞行速度、机翼面积和形状、机翼与气流的相对角度、空气密度等。
说明:补充资料仅用于学习参考,请勿用于其它任何用途。
参考词条