Non-uniform rational B-splines (NURBS) was used to fit component characteristics of aerothermodynamic model for approaching turbine engine.
摘要为了使热力模型更好
逼近涡轮发
机,应用成熟
非均匀B样条来拟合部件特性。
Non-uniform rational B-splines (NURBS) was used to fit component characteristics of aerothermodynamic model for approaching turbine engine.
摘要为了使热力模型更好
逼近涡轮发
机,应用成熟
非均匀B样条来拟合部件特性。
Three-dimensional(3D)unsteady compressible flow over an open cavity and the relevant aeroacoustics are studied using a hybrid LES-acoustic analogy method.
使用大涡模拟-声学比拟相结合方法,研究三维开式空腔
非定常可压缩过流及其相关
声学问题。
The conception model, assembly model and parts model of pneumatic hole impinger are established by the method of intelligent modeling.
采用智能产品建模方法,建立了
潜孔
击器
概念模型、
配模型和零件模型。
Structure of pneumatic material c lamping device and pneumatic system have been introduced with ex-pounding appli cation in a notching press.
介绍对压
结构及
系统,以及
压
在
槽机上
应用。
In this paper, the author proposes a non contact on line measuring and controlling method for external grinding according to the principle of pneutronic measuring.
本文提出一种以测量原理实现
外圆磨削在线无损测控方法。
Spedding and his colleagues think that the unique aerodynamic wake signatures of bat wings are caused by different mechanical operations in the upstroke of the wingbeat.
斯佩丁和他同事们认为,独特
签字后,蝙蝠
翅膀所造成不同
机械操作,在upstroke
wingbeat 。
In Chapter 3, based upon the blade second-order lifting-line model and rotor free-wake model, an analytical method is developed for predicting the rotor wake structure and BVI airload.
基于桨叶二阶升力线理论和旋翼自由尾迹模型,本文在第三章建立了一个适合于直升机旋翼尾迹结构及桨-涡干扰特性分析
方法和模型。
In the third part of the screen the residual water is pressed out of the sludge, at a minimum filter cake thickness, by the pneumatic counterpressure cone at the press discharge.
在屏第三部分,淤泥上残余
水份通过压力排放
反
锥被压出来,形成最低厚度
泥饼状物。
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