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1)  Wave drag
波动阻力
1.
Wave drag and form drag induced by small scale terrain in the nocturnal stable boundary layer;
夜间稳定边界层中小尺度地形激发的形式阻力和波动阻力
2)  pressure drag fluctuation
压差阻力波动
1.
Influence of pressure drag fluctuation on centrifugal pump vibration;
压差阻力波动对离心泵振动影响研究
3)  wave making resistance
兴波阻力
1.
Computation of the wave making resistance of submerged body moving beneath water surface;
潜体近水面航行兴波阻力计算
2.
Calculating the wave making resistance of multi-hull ships based on an integral expression of the Kochin function on the surface panels
单元柯钦函数精确积分的多体船兴波阻力计算
3.
It is indicated that wave making resistance of surface warship can be reduced a lot with a proper bulbous bow by present research based on linear wave making resistance.
试验结果表明,球鼻艏在特定的中高航速下可以使兴波阻力最多减少37%,总阻力最多减少15%。
4)  wave resistance
兴波阻力
1.
Fast method of positional optimization on distance between hulls of a trimaran based on wave resistance;
基于兴波阻力的三体船片体位置快速优化方法
2.
A investigation of wave resistance on the high speed trimarans and their piece hull position optimization;
高速三体船兴波阻力与片体布局优化研究
3.
Solution to wave resistance to trimanan using-Rankine source method of Dawson type;
Rankine源Dawson型方法求解三体船兴波阻力
5)  wave-making resistance
兴波阻力
1.
Research on wave-making resistance simulation of SWATH ships;
小水线面双体船兴波阻力数值仿真研究
2.
A research on numerical prediction method for wave-making resistance and its application to container ship hull form optimization;
兴波阻力数值预报方法研究及其在集装箱船船型优化中的应用
3.
Calculation of wave-making resistance of wave-piercing catamarans by means of linear wave-making resistance theory;
用线性兴波阻力理论计算穿浪双体船的兴波阻力
6)  wavemaking resistance
兴波阻力
1.
The wavemaking resistance of a new type of trimaran-Ovoid-type Hullform,which was proposed by some Japanese researchers,was calculated using a method based on Noblesse s New Slender-ship Theory.
利用该方法计算了卵型船的兴波阻力 ,并将计算结果与实验数据进行比较 ,得到令人满意的结果 。
补充资料:肺循环阻力(或全肺阻力)


肺循环阻力(或全肺阻力)
pulmonary circulation resistance

  血液在肺部血管内流动时和血管壁之间的摩擦力和血液内部的摩擦阻力。肺动脉管壁较薄,分支短而管径大,故肺动脉的可扩性较大,对血流的阻力很小,仅0.12PRU(外周阻力单位)。肺循环动脉部分总的阻力和静脉部分总的阻力相等,故血液流动时在动脉部分的压力降落和静脉部分的压力降落相等。
  
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