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Suprression of shock-induced airflow separation

机译:抑制冲击引起的气流分离

摘要

An apparatus for suppressing shock-induced separation of high speed airflow from a relatively low-energy boundary layer. The apparatus may include an actuator or array of actuators configured to alternately inhale and exhale fluid and positioned to alternately inhale fluid from and exhale fluid into a boundary layer of a fluid mass flowing along the wall. The actuator may be positioned to inhale fluid from a boundary layer separation bubble induced by a supersonic shock wave propagated in the fluid mass.
机译:一种用于抑制震动引起的高速气流与能量较低的边界层分离的装置。该设备可以包括致动器或致动器阵列,该致动器或致动器阵列构造成交替地吸入和呼出流体,并且定位成交替地从沿着壁流动的流体块的边界层中吸入流体和将流体呼出到边界层中。致动器可以定位成从边界层分离气泡中吸入流体,该边界层分离气泡是由在流体块中传播的超音波冲击波引起的。

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