1) distribute load
面力
2) driving face
压力面;受力面
3) interfacial tension
界面张力
1.
Effects of the structure of polyoxypropylene ether surfactants and the salinity of water on oil-water interfacial tension;
聚氧丙烯醚型表面活性剂结构及矿化度对油水界面张力的影响
2.
Influence of viscoelasticity and interfacial tension of non-alkali binary compound solution on recovery efficiency of residual oil after water flooding;
无碱二元体系的黏弹性和界面张力对水驱残余油的作用
3.
Determination of the minimum miscibility pressure of CO-2 and crude oil system by vanishing interfacial tension method;
用界面张力法测定CO_2与原油的最小混相压力
4) surface tension
表面张力
1.
Influences of surface tension of acid solution and contact angle of rock on the cleanup efficiency of surfactant;
表面张力和接触角对酸液助排率的影响研究
2.
Calculation of ternary alloy surface tension with binary alloy segregation factors;
通过二元熔体的偏析因子计算三元合金的表面张力
3.
Liquid surface tension measuring device;
测量液体表面张力的装置
5) Interface tension
界面张力
1.
Effect of interface reaction and interface tension on wettability of Sn-Zn-Bi solders;
界面反应及界面张力对Sn-Zn-Bi焊料润湿性的影响
2.
The experimental results showed that the surface tension and the interface tension of the solution are very low,which indicate that such AFFF solution has a high spreading coefficient and can form a film on oil surface within short time.
试验结果表明,该泡沫溶液的表面张力和界面张力很低。
3.
The effects of the product on the interface tension of ASP system were investigated.
考察了合成产物对三元体系(碱、表面活性剂、聚合物)界面张力的影响。
6) interface stress
界面应力
1.
Theory calculate and finite element analysis of the interface stress in concrete beams strengthened by GFRP;
玻璃钢板加固既有混凝土梁界面应力分析
2.
Based on the displacement function solution for plane issue in elastic mechanics, the common solutions of interface stress and displacement in multilayer coatings system are deduced by Fourier transformation, so that an effective and simple algorithm to calculate interface stress of coatings is obtained.
基于弹性力学平面问题的位移函数解法,运用Fourier积分变换推导了多层涂层体系界面应力及位移分量的一般解,得到一种高效、简便的涂层界面应力计算方法。
3.
As size of low dimensional materials decreases, which leads to the dramatic increase of surface/volume ratio, their properties are essentially controlled by related interface energetic terms, such as interface energy and interface stress.
随着低维材料尺寸的减小,表面体积比急剧增加,界面能和界面应力对材料性能的影响显著增加。
补充资料：举力面理论
用一个附着涡面和尾涡面（即自由涡面）来代替机翼作用的一种理论。主要用于计算机翼的空气动力特性。它是在举力线理论基础上发展起来的。 对于小展弦比、大后掠角的机翼，举力线理论不适用，即不能用一条附着涡线和尾涡面来代替机翼的作用，而应该用一个附着涡面和尾涡面。通常用一些附着涡线近似地代替这个附着涡面。图中画出由速度为V∞的均匀来流、附着涡面和尾涡面构成的理论模型。根据举力面理论可以算出沿翼展的举力分布、机翼上的总举力以及诱导阻力（即由尾涡引起的阻力）等机翼的气动特性。不论举力线理论还是举力面理论,都假定机翼近似位于顺来流的平面内,从而附着涡面（或涡线）和尾涡面都位于同一平面内，尾涡都由后缘拖出，所以这些理论只适用于小攻角（机翼与来流夹角小）的情形。这些理论算出的举力与攻角成正比，有时把它们称为线性理论。当攻角较大或展弦比很小时，涡系就不一定在同一平面内，自由涡不只是从后缘顺流拖出，而且还从前缘、侧缘和翼面上拖出。对于这种情形，可以进一步推广举力面理论，并求出举力和攻角之间的非线性关系。这种推广了的理论称为非线性理论，不属于通常所说的举力面理论。
参考书目
H.Schlichting and E.Truckenbrodt，Aerodynamics of theAirplane,McGraw-Hill,New York,1979.
参考书目
H.Schlichting and E.Truckenbrodt，Aerodynamics of theAirplane,McGraw-Hill,New York,1979.
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