桨叶剖面的英文

• propeller blade section

• "桨叶"英文翻译    awe; paddle
• "剖面"英文翻译    bisect; section; profile
• "对称桨叶剖面" 英文翻译 :    symmetrical blade section
• "复合桨叶剖面" 英文翻译 :    compound blade section
• "拱形桨叶剖面" 英文翻译 :    cambered blade section
• "桨叶剖面尾翘" 英文翻译 :    washback
• "螺旋桨叶剖面" 英文翻译 :    section of screw blade
• "翼型桨叶剖面" 英文翻译 :    airfoil blade section
• "基部充气桨叶剖面" 英文翻译 :    base-vented blade section
• "桨叶剖面阻力系数" 英文翻译 :    blade profile drag coefficient
• "流线型桨叶剖面" 英文翻译 :    streamlined blade section
• "椭圆形桨叶剖面" 英文翻译 :    elliptical blade section
• "螺旋桨叶剖面相对曲度" 英文翻译 :    propeller camber ratio
• "叶剖面" 英文翻译 :    airfoil
• "叶剖面曲度" 英文翻译 :    blade-section camber
• "叶剖面弦" 英文翻译 :    blade-section chord
• "叶剖面最大平均弧高" 英文翻译 :    maximum mean camber of a wing section
• "桨叶片剖面弦长" 英文翻译 :    propeller blade chord
• "桨叶" 英文翻译 :    awe; paddle
• "a-a剖面" 英文翻译 :    a a section; a-a section
• "剖面" 英文翻译 :    [地质学] bisect; section; profile 横剖面 cross section; 纵剖面 longitudinal section; 剖面符号 [图] section symbols; 剖面图 [电磁] sectional view; profile; bisect; profile chart; sectional drawing; section; 剖面线 hatch
• "叶剖攻角" 英文翻译 :    profile angle of attack
• "叶剖厚度" 英文翻译 :    blade section thickness
• "叶剖实投影" 英文翻译 :    true projection of blade section
• "叶剖纵斜" 英文翻译 :    rake of blade section

• Blade profile drag coefficient
  桨叶剖面阻力系数
• At last , a few calculator cases of kinds of section are presented , whose result is proved
  文中还给出了复合材料桨叶剖面特性与试验结果的比较，两者具有较好的一致性。
• Blade section designed based on equivalent operating curve can effectively control the cavitaion area and type , and the desired cavitation performance can obtained
  基于等效运转曲线设计的桨叶剖面能有效地控制空泡范围和空泡类型，得到期望的空泡性能。
• This paper presents a design method of propeller blade section operating in non - uniform flow field and an idea of equivalent operating curve with unchanged cavitations characteristic on blade section , the method for selecting the curve is set up
  摘要给出了非均匀流场中螺旋桨桨叶剖面的设计方法，提出了保持剖面空泡特征不变的等效运转曲线的思想，并创建了等效运转曲线的确定方法。
• To avoid or reduce these trouble induced by the unsteady cavitation , the theoretical design method for propeller and the blade section with the good cavitation performance are adopted to enlarge the cavitation bucket width and control the range and type of the cavitation on the blade . this enables propeller to operate in the non - uniform ship wake rather well
  为了避免或减缓空泡带来的危害，采用螺旋桨理论设计方法和空泡性能优良的桨叶剖面来增加空泡斗宽度和控制桨叶空泡范围及空泡类型，以适应非均匀流场中螺旋桨工作的需要。
• Now , it is important to develop the composite blade researching , two measures including analysis methodology and finite methodology are provided . in this text , the finite rotation composite beam theory developed by hodges and his co - workers , during the late 1980 ' s , is adopted in order to research rotor of helicopter . a liner and two - dimension finite analytic measure is used to calculate the section characteristic and strain of the blade ; a semianalysis methodology is used to calculate the sensitive degree of section characteristic
  以giavotto的线性二维有限元分析模型为基础考虑了复合材料桨叶的结构和变形特点，计入了剖面翘曲的影响，在此基础上编制了具有八节点等参元复合材料桨叶剖面刚度计算的有限元程序，分析计算了复合材料梁的剖面刚度、弯曲中心、剪切中心；并利用半解析法进行剖面刚度、剪切中心、弯曲中心的参数灵敏度分析。