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Investigation on Flow Structures of Supersonic Isolator Flow

机译:超音速隔离器流动结构研究

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An isolator with the cowl convergence angle altering from 0° to 16° and a blockage adjuster installed at the exit to simulate the chocked isolator flow was designed. The investigation of the present isolator configuration via flow visualization and pressure measurement was performed, which was motivated by the need for studying the isolator flow mechanism. Effects of cowl convergence angle and blockage degree were studied experimentally. Both flow visualization and pressure distribution have shown that moderate contraction(β = 4° ~ 12°) provided a favorable entrance condition for isolator starting.
机译:设计了前围板收敛角从0°到16°改变的隔离器,并在出口处安装了堵塞调节器,以模拟堵塞的隔离器流动。通过流动可视化和压力测量对当前的隔离器配置进行了研究,这是由于需要研究隔离器的流动机理而引起的。实验研究了前围板收敛角和阻塞度的影响。流动可视化和压力分布都表明,适度的收缩(β= 4°〜12°)为隔离器启动提供了有利的进入条件。

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