distribution blade

英 [ˌdɪstrɪˈbjuːʃn bleɪd] 美 [ˌdɪstrɪˈbjuːʃn bleɪd]

分散叶片

化学



双语例句

  1. And the gap will undermine the efforts of the pressure distribution on the blade.
    并且间隙的加大会破坏叶片上的压差分布。
  2. The effects of turbomachinery blade bow and sweep on aerodynamic loading distribution of the blade are investigated.
    研究叶轮机叶片的弯扭及掠形等因素对叶片气动负荷分布的影响。
  3. Measurement of global pressure distribution on single blade suction surface at the outlet of cascade wind tunnel
    叶栅风洞出口处孤立叶片吸力面全域压力分布测量
  4. However the presence of hot streak has little effect on the pressure distribution on the blade surface.
    同时进口热斑相对导叶的位置对叶片表面温度的分布也有很大影响。
  5. Whether the distribution of blade induced velocities along the radius can be assumed to be independent of the blade pitch angle of rotors in blade element theory, even for vertical flight;
    叶素理论(即使在处理垂直飞行问题时)中沿半径的诱导速度分布能否认为独立于桨叶安装角分布;
  6. Performance and pressure distribution on blade of highly skewed propellers by using unsteady lifting surface theory
    应用非定常升力面理论计算大侧斜桨性能及桨叶表面压力分布
  7. Prediction of Propeller Characteristics and Pressure Distribution on the Blade by Lifting Line Theory
    用升力线理论预报螺旋桨性能和桨叶表面压力分布
  8. It is shown that the blade bow, twist and leading edge sweep are effective in adjusting the loading distribution on the blade surface.
    分析结果表明,叶轮机叶片的弯扭和前缘掠形对叶片的负荷分布有重要的调节作用。
  9. With the use of holography, the mode, amplitude and phase distribution of gas turbine blade vibration can be determined.
    利用全息照相,我们可以得到燃气轮机叶片振动时的振型、振幅和相位分布。
  10. The effects of nonuniformity of rotor induced velocity distribution and blade flapping elasticity are taken into account and investigated in detail.
    考虑并研究了旋翼诱导速度的一阶谐波分布和桨叶的一、二阶挥舞弯曲模态的影响。
  11. The measured results show that the way is workable, and it is possible to analyze the circulation distribution along the blade span based on the measured tangential velocity distribution at downstream.
    测量结果表明该方案测量导管内流场是可行的,并为导管内螺旋桨叶片的环量分布分析提供了条件。
  12. This paper sets the theoretical and numerical method predicting the unsteady pressure distribution on the propeller blade surface by using perturbation potential based on surface panel method.
    本文建立了扰动速度势面元法预报螺旋桨表面非定常压力分布的理论和数值方法。
  13. Based on the process of energy absorption and distribution between blade and shell, the mechanism of blade with high-speed impacting containment ring was further understood.
    根据撞击过程中能量的分配与吸收,进一步弄清了叶片高速撞击机匣的机理。
  14. On suction surface of positive curved blade, the "C" type static pressure distribution along the blade height is created, and the load of the blade is changed along the blade height and chord, which are the main factors to affect the flow in cascade.
    正弯曲叶片吸力面形成“C”型压力分布,叶片负荷沿叶高和弦长重新分布,这种负荷的重组是弯曲改变叶栅流场的主要因素。
  15. The purpose of this paper is to find out the energy loss mechanism of the curved blade cascades from the static pressure distribution on the blade surface, and to study performance of compressor cascades at different incidences.
    本文试图从叶片表面静压分布来分析弯曲扩压叶栅的能量损失机理,探讨不同弯曲叶片在扩压叶栅中应用的变工况性能。
  16. In the above three situations, the pressure distribution on the blade surfaces and blade tip leakage flows are measured.
    对上述3种工况叶片表面静压分布和叶尖间隙流进行了实验测量。
  17. Finite element analysis of three dimensional steady and unsteady temperature fields ( computation of temperature distribution of turbine blade with composite cooling) numerical analysis of heat transfer and flow with three dimensional steady and transient states in sodium pool of fast breeder reactor
    三维物体稳态及瞬态温度场的有限元分析(复合冷却涡轮叶片三维温度场计算)快堆钠池三维稳态与非稳态流动传热的数值研究
  18. The paper includes four parts: turbulence wind field model, the load of the wind turbine, the load distribution of wind turbine blade, the wind turbine reliability analysis.
    论文包括四部分:紊流风场模型、风力机载荷分析、风力机叶片载荷分布、风力机叶片可靠性分析。
  19. The efficiency distribution along blade span and the inlet and outlet velocity triangle measurement of rotor blades were made around the designing point.
    在设计点附近作了沿叶高效率分布及动叶进、出口速度三角形的测定。
  20. As applications of this method, the propeller's thrust, torque and the pressure distribution on the blade in steady flow are solved. The numerical results are in satisfactory agreement with experiment data.
    本文采用该方法计算了螺旋桨在定常条件下的推力、转矩和叶面压力分布,并与实验结果进行了比较和分析,其结果比较令人满意。
  21. Based on the experimental investigation on the sawing force of concrete, the deflection and stress distribution of saw blade were investigated with finite element analysis, and a new type of diamond blade structure for dry cutting concrete was designed.
    在混凝土锯切过程锯片受力的实验研究基础上,采用有限元方法模拟分析了锯切混凝土过程锯片的变形和应力分布,并优化设计了干切削混凝土用锯片的结构及其参数。
  22. A numerical method is presented for prediction of propeller performance and pressure distribution on blade surface according to lifting surface theory.
    本文提供了一种根据升力面理论计算螺旋桨桨叶表面压力分布和螺旋桨性能的数值方法。
  23. This technique can be used to design the blade profile with prescribed dimensionless velocity distribution at the suction and pressure surface. Depending on comparing the aimed velocity distribution with the calculated velocity distribution, the new blade was obtained by modifying the blade profile shape.
    应用这一技术设计叶型,规定叶片表面无量纲目标速度分布,通过比较目标速度分布和计算获得的速度分布来修改叶片压力面和吸力面的坐标,最终获得要求的叶片形状。
  24. Research on Optimization of Blank Allowance Distribution for Blade Parts
    叶片零件毛坯余量分布优化问题研究
  25. A suit of optimization program have been designed, through the influence disciplinarians research of velocity distribution of blade surface and the shape of blade profile, optimization blade profile have been obtained through adjust the velocity distribution available.
    通过研究叶片表面速度分布对叶型形状的影响规律,设计出了一套优化程序,通过有效调节叶片表面速度分布获得了优化的设计叶型。
  26. The aerodynamic optimization of a transonic fan rotor was implemented by controlling the BVF ( boundary vorticity flux) distribution on rotor blade. A novel objective function of torque associated with BVF was used to optimize the blade configuration.
    将加功量作为目标函数并结合边界涡量流BVF(BoundaryVorticityFlux)这个诊断因子,对某高性能跨声风扇转子进行了优化。
  27. Finally, the total loss distribution along the blade span of the axial flow compressor is estimated according to an improved end wall loss model and a shock loss model.
    再应用改进了的端壁损失和激波损失模型,最终算出轴流压气机设计点损失沿叶高的分布规律。
  28. The stress distribution and deformation of blade was obtained finally.7.Simulation analysis on soil cutting process by cutting blade was carried out. The soil cutting principle was further revealed.
    对螺旋叶片边缘焊接的切土刀片进行了切土过程数值模拟,深入揭示了其切土机理,得到了其应力分布和变形情况。
  29. Controlling loading distribution method is a kind of design method of blade shape line by adjusting the loading distribution on the blade surface.
    控制载荷法是一种通过控制叶片表面载荷分布方式来设计叶片型线的方法。
  30. The increment of blade length makes the equal work distribution along the blade length be unable to dig the potential power of long blade at the part with high circumferential velocity.
    叶片高度的增长,使沿叶高的等功设计已经不能充分发挥长叶片高圆周速度部分的做功能力。