非设计点的英文

• off design point
• off-design point

• "非"英文翻译    mistake; wrong; errors
• "设计"英文翻译    devise; project; plan; desig ...
• "点"英文翻译    drop
• "设计点" 英文翻译 :    design point; point; design
• "设计点设计" 英文翻译 :    point design
• "非设计的" 英文翻译 :    off design; off-design
• "非设计工况" 英文翻译 :    off design conditions; off-design behaviour; off-design conditions
• "非设计情况" 英文翻译 :    off-design condition
• "非设计特性" 英文翻译 :    out-of-rig characteristics
• "非设计条件" 英文翻译 :    off design condition; off-design condition
• "非设计性能" 英文翻译 :    off design performance; off-design performance
• "非设计状态" 英文翻译 :    off-design conditions
• "变设计点法" 英文翻译 :    variable design point method
• "设计点效率" 英文翻译 :    design point efficiency; design-point efficiency
• "设计点性能" 英文翻译 :    point performance
• "非设计马赫数" 英文翻译 :    off-design mach number
• "单设计点飞机" 英文翻译 :    single-design-point aircraft
• "双设计点飞机" 英文翻译 :    two-design-point aircraft
• "设计点,设计工况,计算点" 英文翻译 :    design point
• "非设计的；非计算的" 英文翻译 :    off-design
• "非设计工况排水量" 英文翻译 :    off-design displacement
• "非设计工况性能" 英文翻译 :    off-design performance
• "非设计工作规范" 英文翻译 :    off design behavior; off-design behavior; off-design behaviour
• "非设计状态的特性" 英文翻译 :    off-design behavior
• "非设计状态排水量" 英文翻译 :    off design displacement

• The software fluent was employed and the two - dimensional flow field and performance parameters of four hypersonic / inlet models at design and off - design condition are obtained
  采用fluent软件对所设计的进气道设计点和非设计点二维流场和性能进行了数值模拟。
• Firstly , the performance is calculated at the design point of the ws - 9 aeroengine by using the numerical model established . secondly , after obtaining the performance coupling parameters , the steady - state performance of the non - designed points is caculated . third , respectively make the limitation of rotate speed of the high pressure rotor and low pressure rotor equal to corresponding parameters of designed point , after the data calculated compared with those of designed point and actual testing of the manufactory , the error is obtained
  首先，用所建立的发动机数学模型计算了发动机在设计点的各项性能，第二，根据发动机各部件的耦合特性参数计算得到发动机在非设计点状态下的各项稳态性能，第三，分别设定限制高压转子转速和低压转子转速逼近设计点条件下对应的参数，将计算得到的性能数据与设计点性能进行了比较，并将非设计点的计算结果与生产试车过程实测的性能数据进行对比，给出了该稳态模型计算结果与实际试车数据的误差。