环形扩压器造型计算方法
A METHOD FOR CONFIGURATION OF ANNULAR DIFFUSER
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摘要: 以往的计算方法常不计沿程压力损失对造型的影响,且认为流面与发动机中心线垂直。计算表明当扩压器进出口中心流线差较大时,计算误差较大。本文则考虑了沿程压力损失,且认为流面与扩压器中心流线垂直,给出了一种新的扩压器造型计算方法。Abstract: A new method for calculation of annular diffuser configuration is offered, which takes pressure loss and perpendicularity of air-through section to the center airflow-line into consideration. When there exists large declination of center flow-lines at inlet and exit,this method is more reasonable than the conventional one which ignores these two factors.
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