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Airfoil performance modification using synthetic jet actuators

机译:使用合成射流执行器改变机翼性能

摘要

Systems and methods for modifying fluid flowing over solid bodies are provided. A representative system incorporates a vorticity concentration-producing component and a synthetic jet actuator. The vorticity concentration-producing component is disposed on a pressure side of the solid body. The fluid flowing over the solid body remains attached to a surface of the solid body in a vicinity of the vorticity concentration-producing component. The synthetic jet actuator includes a jet housing that incorporates an internal chamber with a volume of fluid and an opening in the jet housing connecting the internal chamber to an external environment having the fluid. The synthetic jet actuator is operative to periodically change the volume within the internal chamber such that a synthetic jet stream comprising a series of fluid vortices is generated and projected in the external environment out from the opening of the jet housing resulting in a reduction in pressure drag of the solid body compared to the pressure drag exhibited by the solid body without operation of the synthetic jet actuator.
机译:提供了用于改变流经固体的流体的系统和方法。代表性系统结合了产生涡度浓度的组件和合成射流致动器。产生旋涡浓度的组分设置在固体的压力侧。在固体上流动的流体在产生旋涡浓度的成分附近保持附着在固体表面上。合成喷射致动器包括喷射器壳体,该喷射器壳体结合了具有一定体积的流体的内部腔室和在喷射器壳体中的将内部腔室与具有流体的外部环境连接的开口。合成射流致动器可操作以周期性地改变内部腔室内的容积,从而产生包括一系列流体涡流的合成射流,并在外部环境中从射流壳体的开口中射出,从而降低了压力阻力与在没有合成射流致动器的操作的情况下固体所表现出的压力阻力相比,固体的压力减小了。

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