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口板的英文

发音:  
"口板"怎么读用"口板"造句

英文翻译手机手机版

  • buccal plate
  • hypostomata
  • hypostome
  • labra
  • labrum
  • oral plate(orals)

例句与用法

  • Sli : synchronous line optical interface
    同步线路光口板
  • It can increase the hole inclination angle range and drill elevation angle hole , while setting the top drive power head and hole top plate toward the opposite direction
    4钻机动力头及孔口板调转方向,可钻凿仰孔。
  • It can increase the hole inclination angle range and drill elevation angle hole , while setting the top drive head and hole top plate toward the opposite direction
    动力头及孔口板调转方向,可直接钻凿仰孔,大大增加钻孔倾角范围。
  • It can increase the hole inclination angle range and drill elevation angle holes , while setting the top drive power head and hole top plate toward the opposite direction
    动力头及孔口板调转方向,可直接钻凿仰孔,大大增加钻孔倾角范围。
  • The application program for t he new digital system is based on windows nt workstation 4 . 0 operating system and it was developed under visual c + + 5 . 0 applying ooa and ood
    为适应测控软件的实时性和可靠性要求,我们运用microsoft公司的ddk设备驱动程序开发包研制了pcl - 731并口板与ad / da转换板的设备驱动程序。
  • A parametric analysis of the inviscid effects of leading edge sweep , sidewall compression , width - height ratio , cowl position and inflow mach number on spillage is finished . numerical simulations are completed for a series of inlets at various flight height and velocity . the research indicates that the area of spillage window , which is mainly determined by the position of the cowl , significantly influences the spillage characteristic of the scramjet inlet
    阐明了侧板后掠的侧压进气道设计参数对构型溢流影响;对不同侧板配置方式的侧压式进气道进行了数值模拟,通过对比分析,发现由唇口板的位置所决定的溢流窗面积的大小对进气道溢流特性的影响显著。
  • In this thesis , hypersonic sidewall compression inlet ' s self - starting characteristics are numerical simulated and tested . with increasing mach number of inflow gradually , the hypersonic sidewall compression inlets can self - start . compared with the hypersonic sidewall compression inlet starting directly , characteristics are different . moving cowl , decreasing interior contraction ratio also can realize the hypersonic sidewall compression inlet ' s self - starting because of separation bubble on sidewall spilling out
    其次,在数值模拟结果的基础上,设计了实验模型和装置并在马赫3 . 85的风洞中进行了移动唇口板减小内收缩比实现侧压式进气道自起动的风洞实验,验证了数值模拟的结果。
  • It is no effect on a sidewall compression inlet ' s starting characteristics while a starting sidewall compression inlet is moved cowl to increase interior contraction ratio appropriately . back pressure effect on characteristics of self - starting for hypersonic sidewall compression inlet is tested in mach 3 . 85 wind tunnel . the hypersonic sidewall compression inlet with interior contraction ratio 1 . 24 can self - start . unstart hypersonic sidewall compression inlet caused by high back pressure can self - start by moving cowl to decrease interior contraction ratio
    最后,实验研究了反压对侧压式进气道自起动特性的影响,内收缩比1 . 24的侧压式进气道可以实现自起动并且实验验证了由于反压过高而不起动的侧压式进气道,通过移动唇口板以减小内收缩比可以实现侧压式进气道的自起动。
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