声速流的英文

• sonic flow

• "声速"英文翻译    acoustic velocity; acoustic ...
• "超声速流" 英文翻译 :    supersonic flow; ultrasonic flow
• "高超声速流" 英文翻译 :    hypersonic speed flow
• "跨声速流" 英文翻译 :    transonic flow
• "跨声速流场" 英文翻译 :    transonic flow field
• "亚声速流" 英文翻译 :    flow at su onic velocity; flow at subsonic velocity; su onic flow; subsonic flow
• "超声速流[动]又称“超音速流[动]”。" 英文翻译 :    supersonic flow
• "跨声速流[动]又称“跨音速流[动]”。" 英文翻译 :    transonic flow
• "亚声速流[动]又称“亚音速流[动]”。" 英文翻译 :    subsonic flow
• "超声速流检测器" 英文翻译 :    ultrasonic flow detector
• "特超声速流状态" 英文翻译 :    hypersonic flow condition
• "亚声速空气动力学；亚声速流" 英文翻译 :    subsonics
• "亚临界流；次临界流；亚声速流" 英文翻译 :    subcritical flow; sub-criticalflow
• "高超声速流[动]又称“高超音速流[动]”。" 英文翻译 :    hypersonic flow
• "声速" 英文翻译 :    acoustic velocity; acoustic speed; [物理学] sound velocity; sonic velocity
• "变速流" 英文翻译 :    non uniform flow; nonuniform flow; variable flow; varied flow; varying flow
• "等速流" 英文翻译 :    uniform current; uniform flow
• "低速流" 英文翻译 :    low-speed flow
• "高速流" 英文翻译 :    high eed flow; high speed flow; high-speed stream; high-velocity current
• "加速流" 英文翻译 :    accelerated flow; accelerating flow; expedited flow
• "减速流" 英文翻译 :    antitriptic current; decelerated flow; decelerating flow; decererating flow; retarded flow
• "失速流" 英文翻译 :    stalled flow
• "速流的" 英文翻译 :    fast flow
• "音速流" 英文翻译 :    sonic flow; sonic stream
• "超声速" 英文翻译 :    hypersonic speed; superacoustic; supersonic eed; supersonic speed; supersonic velocity; supersonics; ultrasonic speed; ultrasonic velocity; ultrasound velocity

• Numerical simulation of transonic flow field in two turbine cascades
  两个涡轮叶栅跨声速流场的数值模拟
• Flow at subsonic velocity
  亚声速流
• The cell - centred finite volume algorithm , nnd finite volume algorithm and ausm + finite volume algorithm are studied for solving the euler equations , their abilities for hypersonic problem are studied especially
  本文分别对格心有限体积格式、 nnd有限体积格式和ausm +有限体积格式进行了研究，在求解euler方程的基础上，研究了它们对跨音速以及高超声速流场计算问题的解决能力。
• But the nnd algorithm can " t reach 2 - order precision , and the cell - centred finite volume algorithm is not suit to solve hypersonic problem . for the efficiency of the four - stage runge - kutta time - stepping scheme is low , and the robust is bad for the hypersonic problem , an implicit time - stepping scheme is adopted . this scheme can preserve the results precision and improve the computing efficiency sharply , and is an innovation for the time - stepping scheme of unstructured grid
  为了解决目前传统四步龙格一库塔时间推进效率较低、计算高超声速流场时鲁棒性较差的问题，本文改进并采用了一种隐式时间推进格式，能够在保证精度要求的情况下有效的提高流场计算时的计算效率，对基于非结构网格的时间推进格式有了发展和创新。