升力面的英文

音标：[ shēnglìmiàn ] 发音:

"升力面"怎么读用"升力面"造句

英文翻译手机版

carrying piston
lift airfoil
lifting surface
lifting-piston
plane surface
supporting piston
supporting surface

"升力"英文翻译 elevating force; lift force; ...
"面"英文翻译 face
"导管升力面" 英文翻译 : nozzle lifting surface
"机身升力面" 英文翻译 : fuselage lifting surfaces
"前体升力面" 英文翻译 : forebody lifting surface
"全部升力面" 英文翻译 : complete lift surface
"扇形升力面" 英文翻译 : lifting quadrant
"升力面(螺桨)" 英文翻译 : lifting surface
"升力面颤振" 英文翻译 : lifting surface flutter
"升力面积" 英文翻译 : lifting area; supporting area
"升力面理论" 英文翻译 : lifting surface theory; lifting-plane theory; lifting-surface
"升力面面积" 英文翻译 : lifting surface area
"升力面载荷" 英文翻译 : lifting area load
"旋转升力面" 英文翻译 : rotating lifting surface
"圆环升力面" 英文翻译 : annular lifting surface
"主升力面" 英文翻译 : main lifting surface; main-surface airfoil
"总升力面积" 英文翻译 : total lifting area
"升力面理论解" 英文翻译 : lifting-surface solution
"升力面上的怜" 英文翻译 : flow at the lifting surface
"亚音速升力面" 英文翻译 : subsonic lifting surface
"超音速升力面理论" 英文翻译 : supersonic lifting-surface theory
"非定常升力面理论" 英文翻译 : unsteady lifting surface theory
"空气动力升力面" 英文翻译 : aerodynamic lifting surface
"升力面下洗流场" 英文翻译 : downwash field for lifting plane
"亚音速升力面理论" 英文翻译 : subsonic lifting-surface theory

例句与用法

Aerodynamic lifting surface
空气动力升力面
Flow at the lifting surface
升力面上的怜
Lifting surface theory
升力面理论
Zhang jian - hua , wang guo - qiang . prediction of hydrodynamic performances of ducted controllable pitch propellers [ j ] . journal of ship mechanics , 2002 , 6 ( 6 ) ( accepted )
王国强,胡寿根.螺旋桨非定常性能计算的升力面方法[ j ] .上海交通大学学报, 1989 ( 3 )
The blade section can be designed by parent section , thereby its chordwis circulation distributions can be worked out , and then lifting surface theory is used to design the three dimension blade geometry
剖面采用母型剖面方法来设计，进而可确定桨叶弦向环量分布，然后由升力面理论设计三维桨叶的几何形状。
Numerical lifting - surface theory has been developed as a practical tool in predicting marine propeller ' s hydrodynamic performance because it is easily being computed and accurate for application
升力面理论由于方法简单易行，它可以对螺旋桨的水动力性能作出非常准确的预报，是当前求解螺旋桨的水动力性能有力的分析工具。
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。
In the second part , firstly , the mathematical model for predicting hydrodynamic characteristics of varivec propeller under steady or unsteady condition are present , based on the general propeller lifting - surface theory , potential flow theory and green theorem . then , theoretical calculation methods for predicting hydrodynamic characteristics of varivec propeller designed above paragraphs are present , based on the finite basic solution method , the unsteady vortex lattice method and hess - smith method
在理论计算部分，本文首先基于常规螺旋桨升力面理论、势流理论和格林定理建立了定常和非定常状态下全方向推进器水动力性能计算的数学模型，然后利用有限基本解法、非定常涡格法和赫斯?史密斯方法对全方向推进器定常和非定常状态下的数学模型进行了数值离散，接下来针对前面所设计的全方位推进器进行了数值预报。
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。
In lifting - surface theory , the non - liner phenomena of the trailing vortex in the transition wake area and of the tip vortex separation are considered . in surface panel method hyperboloidal quadrilateral panels are employed and the morino ' s analytical formulation is used to determine the influence coefficients . the more reasonable pressure kutta condition is satisfied at the trailing edge of propeller blade
在计算中，对于升力面理论，本论文考虑了过渡区尾涡收缩和叶梢分离的非线型现象的影响；对于面元法，本论文采用的是计算较为简便的基于扰动速度势的基本公式及双曲面形状的面元，在桨叶随边满足更趋合理的压力kutta条件，并用morino导出的解析公式计算面元的影响系数的快速有效的数值预报方法。