前缘驻点的英文

• leading edge stagnation

• "前缘"英文翻译    lip; snoot; leading edge
• "驻"英文翻译    stay; halt; stop
• "点"英文翻译    drop
• "驻点" 英文翻译 :    arrest point; critical point; stagnation point; stationary point
• "前缘" 英文翻译 :    lip; snoot; leading edge
• "后驻点" 英文翻译 :    rear stagnation point
• "前驻点" 英文翻译 :    forward stagnation point
• "热驻点" 英文翻译 :    thermal arrest
• "驻点的" 英文翻译 :    stagnant
• "驻点解" 英文翻译 :    stagnation point solution
• "驻点流" 英文翻译 :    stagnation flow; stagnation point flow
• "驻点能" 英文翻译 :    stagnation energy
• "驻点线" 英文翻译 :    attachment line
• "钝头驻点" 英文翻译 :    blunt stagnation point
• "非驻点传热" 英文翻译 :    non-stagnation point heat transfer
• "前驻点流线" 英文翻译 :    forward stagnation streamline
• "前驻点线" 英文翻译 :    front attachment line
• "下表面驻点" 英文翻译 :    lower-surface stagnation point
• "轴对称驻点" 英文翻译 :    axially symmetric stagnation point
• "驻点表面" 英文翻译 :    stagnation surface
• "驻点测量" 英文翻译 :    stagnation point measurement
• "驻点超压" 英文翻译 :    stagnation overpressure
• "驻点传热" 英文翻译 :    stagnation point heat transfer
• "驻点激波层" 英文翻译 :    stagnation-point shock layer
• "驻点流线" 英文翻译 :    stagnation streamline

• The method of prediction the discharge coefficients of film cooling holes on the turbine blade suggested by d . a . rowbury et . al has been improved in this paper to fit the computations in the cases of low pressure ratios and the holes in leading edge region especially . the effects of external cross - flow , hole geometry and reynolds number in the hole were taken into account . an additive loss coefficient method is subsequently applied to the test data in order to assess the effect of the external cross - flow
  Rowbury等提出的流量系数工程算法进行了改进，计算结果和实验数据的比较表明改进后的新模型使低吹风比和前缘驻点附近流量系数的计算得到了明显的改进，而在高吹风比下仍能保持与实验数据相符，这种算法有可能成为低压比情况下型面气膜冷却的一种通用设计方法。