侧斜的英文

• shew

• "侧"英文翻译    slant; sloping
• "斜"英文翻译    oblique; slanting; skew; bev ...
• "侧斜肌" 英文翻译 :    lateral oblique muscle
• "侧斜角" 英文翻译 :    angle of skew back; side rake angle
• "侧斜位" 英文翻译 :    lateral oblique position
• "侧斜线" 英文翻译 :    skew line
• "侧斜仪" 英文翻译 :    dip circle; driftmeter
• "背侧斜角肌" 英文翻译 :    m. scalenus dorsalis
• "臂侧斜上举" 英文翻译 :    arms half side upward
• "臂侧斜下举" 英文翻译 :    arms half side downward
• "侧斜冰碛层" 英文翻译 :    lateral moraine
• "侧斜端砖" 英文翻译 :    end-skew on edge
• "侧斜负荷" 英文翻译 :    side loading
• "侧斜螺旋桨" 英文翻译 :    skewed propeller
• "侧斜位投照" 英文翻译 :    oblique lateral projection
• "侧斜叶廓" 英文翻译 :    skew-back profile
• "吊式侧斜仪" 英文翻译 :    hanging clinome ter
• "腹侧斜角肌" 英文翻译 :    m. scalenus ventralis
• "桨叶侧斜" 英文翻译 :    skewback
• "桨叶侧斜的" 英文翻译 :    skew
• "两侧斜视" 英文翻译 :    bilateral strabismus; bilateralis strabismus
• "上侧斜面" 英文翻译 :    bezel facet; bezelfacet
• "实效侧斜角" 英文翻译 :    effective skew angle
• "实效侧斜线" 英文翻译 :    effective skew line
• "有效侧斜" 英文翻译 :    effective skew

• Prediction of hydrodynamic performance of highly skewed propeller
  大侧斜螺旋桨水动力性能预报
• Hanging clinome ter
  吊式侧斜仪
• Hd propellers are a type of marine propellers having new blade sections , moderate skew and a small area - ratio , with the virtues of higher efficiency , lower vibration and noise and lighter weight
  沪东型( hd )螺旋桨是一种新型的叶剖面、中等侧斜、小盘面比的螺旋桨。它具有效率高、振动和噪音低、重量轻等优良性能。
• They have also been exported to iran , china , india , poland , romania and algeria . china has two type 636 submarine which are designed for antisubmarine and anti - surface ship asuw warfare as well as for general reconnaissance and patrol missions
  636型潜艇是在877型的基础上又进行了改进提高，其降低动力装置的转速，采用了七叶大侧斜螺旋桨，增大充电功率提高了充电能力，改进降噪措施，进一步降低了噪声。
• At varying conditioning - test stimulus intervals , segmental conditioning stimulus was applied in the tibialis anterior muscle ipsilateral and contralateral to the test stimulus , and heterosegmental conditioning stimulus was applied in the contralateral trapezius muscle to modulate the nwr
  检测同侧和对侧的胫骨前肌在刺激间隔、节段性制约刺激变化情况下的测试参数、异源节段性制约刺激作用于对侧斜方肌以调整nwr 。
• Using a combination method of the lifting surface theory and acoustic technique , the effects of different diameters , skews and rakes on the discrete noise of the propeller are studied by the numerical method and some useful results for engineering are presented in this paper
  利用升力面理论和声学方法得到的离散谱噪声的预报公式，对螺旋桨直径、侧斜、纵倾变化对离散谱噪声的影响作了数值计算，并得到了工程上有实用意义的结果。
• The paper has improved the existing lifting - line and lifting - surface design method by including the rake and skew and solving the optimum circulation distribution with the optimum theory . the blade geometry is expressed with b - spline for the lift - surface method . the boundary condition on the blade is transformed to minimize the summation of the square of normal velocities , the fair blade geometry can be obtained by present technique and the design quality is better
  改进了现有的升力线和升力面设计方法，在升力线设计中计及桨叶的纵倾和侧斜的影响，用优化理论求解最佳环量分布，升力面设计中用b样条来拟合桨叶，将物面边界条件转化为求法向速度分量的平方最小，由此可得到光顺的桨叶几何形状，提高和改进了设计质量。
• The surface panel method has been applied to predict the hydrodynamic performance of highly skewed propeller . the surface of propeller and its trailing vortex are discreted by a number of small hyperboloidal quadrilateral panels with constant source and doublet distribution . for highly skewed propeller , the conventional method generating grid oriented along constant radii will result in a high aspect ratio and a high skewness and a twist panel near the propeller tip on blade surface , which result easily in incorrect calculation results of velovity on blade surface , even in iteration divergence and calculation failure . a “ non - conventional grid ” is developed to acoid these problems . this grid can effectively solve the problem of the calculation and convergence for highly skewed propeller . the non - linear kutta condition of equal pressure on upper and lower at the trailing edge is executed by the iterative procedure . by sample calculating , the obtained results are satisfied the experimental data
  采用面元法预报大侧斜螺旋桨水动力性能，螺旋桨表面及尾涡面离散为四边形双曲面元，每个面元上布置等强度源汇和偶极子分布.对于大侧斜螺旋桨而言，桨叶表面采用常规的等半径网格划分方法在近叶梢处将导致大展弦比、大侧斜和扭曲面元，这容易使桨叶表面速度的计算结果不正确，甚至会导致迭代过程发散及计算失败.文中建立了一种“非常规网格”划分方法，能有效地解决大侧斜螺旋桨的计算和收敛问题.桨叶随边处通过迭代实现非线性等压库塔条件