Chinese translation for "vortex lattice"
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- 涡串
涡流栅格
涡旋点阵
Related Translations:
- Example Sentences:
| 1. | The vortex lattices of anisotropic superconductors in the bcs mechanism
机制下各向异性超导体的涡旋格子 | | 2. | Study of the rudder with additional thrust fins used by non - linear vortex lattice method
非线性涡格法预报桨后舵附推力鳍水动力性能 | | 3. | As being superfluid , particle current in bec is irrotational and this makes that its respondence to rotation is different from rotating as a whole for usual fluid and is to form a vortex or vortex lattice
作为超流体， bec中的粒子流是无旋的，这使得它对旋转的响应异于普通流体的整体转动而产生涡旋或涡旋晶格。 | | 4. | In the first part , the steady nonlinear vortex lattice method is adopted to calculate the hydrodynamic characteristics of open water ichthyoid rudder , and the induced velocity of ichthyoid rudder is calculated using panel method
本文理论计算部分，采用定常非线性涡格法计算鱼形舵的水动力性能，用面元方法计算舵流场的诱导速度。 | | 5. | 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。 | | 6. | Based on the green ' s formula and the assumption of the propeller blade ' s thin sections , a lifting - surface method of propellers with the vortex lattice and equal source panel distributions on the mean camber surface has been introduced for the prediction of steady propeller ' s hydrodynamics in this paper . an approximate kurta condition was applied
基于creen公式和薄翼理论假设导出的升力面方法，采用在螺旋桨拱弧面上分布离散涡、源布置方法预报均匀流场中的螺旋桨的定常性能，螺旋桨尾涡面上压力连续性条件采用近似的kutta条件处理。 | | 7. | On the base of the soft about the deformation of aerodynamic configuration of mav , the advanced controlling technique of the deformation o f aerodynamic configuration about the prototype mav will be explored . based on the characteristic of micro air vehicle , this paper abstracted the aerodynamic evaluation mathematics models , developed a aerodynamic engineering estimation program , all kinds of aerodynamic configuration was compared and analyzed , found the perfect configuration and got the prototype of mav . abstracted the model about the deformation of aerodynamic configuration on base of the method of vortex lattice , developed the program for researching the performance of the deformation of aerodynamic configuration
本文针对mav的具体特点，抽象出mav的气动工程计算数学模型，建立起气动工程估算环境，对各种气动布局进行了气动特性比较分析与综合，寻求出理想的mav气动布局方案并提出mav原型机，抽象出基于涡格法的气动外形形变的数学模型，建立起气动外形形变性能研究环境，探讨新型的飞行控制方法和气动力控制策略，在得出气动外形形变模型的初始方案后，对其进行进一步的优化，最后得出理想的气动外形形变执行机构组合阵列。 |
- Similar Words：
- "vortex interaction" Chinese translation, "vortex interference" Chinese translation, "vortex interference effect" Chinese translation, "vortex invariant" Chinese translation, "vortex kinetics" Chinese translation, "vortex lattice method" Chinese translation, "vortex layer" Chinese translation, "vortex lift" Chinese translation, "vortex line" Chinese translation, "vortex line distribution" Chinese translation
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