空气动力特性的英文

• aerodynamic behavior
• aerodynamic characteristics
• aerodynamic properties
• aerodynamical properties
• aerodynamics
• air characteristics

• "空气"英文翻译    air; atmosphere
• "动力"英文翻译    motive power; power; dynamic
• "特性"英文翻译    characteristic; character; p ...
• "风轮空气动力特性" 英文翻译 :    aerodynamic chatacteristics of rotor
• "基本空气动力特性" 英文翻译 :    primary aerodynamic characteristics
• "空气动力特性分析" 英文翻译 :    aerodynamic analysis
• "空气动力特性曲线" 英文翻译 :    aerodynamic characteristic curve
• "空气动力特性图" 英文翻译 :    aerodynamic nomogram
• "空气动力特性研究" 英文翻译 :    aerodynamic investigation
• "理论空气动力特性" 英文翻译 :    calculated aerodynamic characteristics
• "模拟空气动力特性" 英文翻译 :    analoged aerodynamics
• "气动力特性" 英文翻译 :    aerodynamic characteristics
• "弹性翼空气动力特性" 英文翻译 :    elastic-wing aerodynamic characteristics
• "定常运动的空气动力特性" 英文翻译 :    static aerodynamic characteristic
• "非线性空气动力特性" 英文翻译 :    nonlinear aerodynamic characteristic
• "非线性空气动力特性曲线" 英文翻译 :    nonlinear aerodynamic characteristic
• "空气动力特性的非线性" 英文翻译 :    aerodynamic nonlinearity
• "空气动力特性的改善" 英文翻译 :    aerodynamic refinement
• "空气动力特性列线图" 英文翻译 :    aerodynamic nomogram
• "空气动力特性最优化" 英文翻译 :    aerodynamic optimization
• "线性空气动力特性曲线" 英文翻译 :    linear aerodynamic characteristics
• "有翼导弹空气动力特性" 英文翻译 :    aerodynamic characteristics of winged missile
• "增升装置空气动力特性" 英文翻译 :    aerodynamics of high-lift devices
• "考虑空气粘性的空气动力特性" 英文翻译 :    viscous-aerodynamic characteristics
• "原始气动力特性" 英文翻译 :    primary aerodynamic characteristic

• The dynamic performance of a ram air system will vary with mach number and altitude and this tends to follow the aerodynamic characteristics of the missile .
  像导弹空气动力特性一样，冲压空气式系统的动态特性随马赫数和高度的变化而变化。
• Motrcycles . controllability and stability . teminology . aerodynamic characteristics
  摩托车操纵稳定性术语空气动力特性
• Methods for testing and rating induction units for air distribution systems - thermal and aerodynamic performance
  空气分配系统用感应装置试验及评定方法.第1部分:热特性和空气动力特性
• Methods for testing and rating terminal reheat units for air distribution systems - thermal and aerodynamic performance
  空气分配系统终端再热装置试验与评定方法.第1部分:热性能及空气动力特性
• So considering the influence of the aerodynamics on vehicle has become more important in vehicle research and design
  而考虑空气动力特性对车辆行驶的影响，特别对操纵稳定性的影响尤其重要。
• After compared with the results without regard to aerodynamics and the experiment results , i think the numeric simulati on is exact and method is correct and effective
  在分别与未考虑空气动力特性时和试验结果作比较之后，说明数字模拟是比较准确的，仿真方法是准确有效的。
• The aerodynamics characteristic of spinning projectile with lateral jets has constitutionally difference in formation from that without jet , and it waves periodically . these characteristics are very important for the study of aerodynamics of projectile with lateral jets
  与光弹体相比，旋转侧喷弹丸的空气动力特性不仅在形成机理上发生了本质变化，而且在数值上表现出复杂的波动形式，这些特点将对旋转侧喷弹丸空气动力研究带来直接和深远的影响。
• Compared with a delta wing aircraft , the double - delta wing configuration has better aerodynamic performance at high angles of attack . an operational analysis was introduced as a method for evaluating training effectiveness of trainer aircraft . approaches to the engineering estimation of aerodynamic characteristics for aircraft with a double - delta wing configuration were studied , and the procedures for determining aircraft performance indices formulated . taking training effectiveness as the objective function and geometric parameters of the wing platform as design variables , through a numerical multivariate optimization arithmetic , the conceptual design optimization for a certain fighter trainer aircraft with double - delta wing configuration was carried out under the constraints of tactical and technical requirements and interrelated geometry . agreement of a calculation example with engineering practice indicates that the optimal design has higher training effectiveness than the baseline design , and in addition , improves the structural force - bearing conditions
  双三角翼气动布局比三角翼飞机具有更好的大攻角空气动力特性.引入了评估教练机训练效能的作战分析法,研究了双三角机翼布局飞机空气动力特性的工程计算途径以及飞机性能指标的确定方法.以训练效能作为目标函数并选取机翼平面形状的几何参数为设计变量,采用多变量数值寻优方法,在战术技术指标及相关几何约束条件下,对某高级教练机的双三角机翼气动布局方案进行了优化选择.算例表明最优方案不仅比原准方案具有更高的训练效能,还改善了结构的受力情况,与工程实践吻合
• According to the measuremental data of the two ammunications , the anti - designed computation and analysis of aerodynamic characteristic , flight stability , exterior ballistic characteristic for the two ammunications are studied with the advanced methods of the exterior ballistics . using the monte calo algorithm , the statistic mathematical model about ammunication ' s intensity is established and the 1000 miter vertical target intensity and the fall intensity are discussed in detail for the two ammunications . the improval potential and the main technical approachs of these ammunication ' s exterior ballistic performances are presented by compositive optimal algorithm
  根据工厂对俄ak130舰炮弹药的测绘数据，利用先进的外弹道数值分析方法对两种弹药的空气动力特性、飞行稳定性特性、外弹道特征量等进行了反设计计算分析；采用montecarlo方法，建立了舰炮弹药密集度性能统计分析数学模型，对两种弹药的立靶密集度和地面密集度进行了详细的计算分析；利用外弹道性能综合优化设计方法对两种弹药的外弹道性能指标的改进潜力和主要技术途径进行了分析。
• 3 . the aerodynamic characteristics and mechanism of flight dynamics under the condition of post - stall maneuvers are discussed , and then the inputs of adaptive fuzzy system are determined . using the control law and nonlinear motion equations built above , some typical post - stall maneuvers are simulated and the effects of thrust vectoring on post - stall maneuver are analyzed
  3 、讨论了过失速机动条件下的空气动力特性和飞行力学机理，在此基础上对自适应模糊逻辑系统的输入进行了分析，确定了自适应模糊逻辑系统的输入。