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Development of design methodology for a synthetic jet actuator array for flow separation control applications

机译:用于流分离控制应用的合成射流致动器阵列的设计方法开发

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This article documents the development of synthetic jet actuator array hardware to augment high-lift system effectiveness in a wind tunpel model. The study involved the design, manufacture and bench test of a synthetic jet actuator array based on an inclined actuator configuration to reduce volume installation requirements without a loss in jet velocity relative to a non-inclined baseline model; incorporation of proper synthetic jet actuator systems wiring and internal synthetic jet actuator chamber pressure-sensing for actuator health monitoring. The peak velocity obtained from the inclined synthetic jet actuator array was 100m/s, which favourably compares to the baseline array (~90m/s), while reducing the usable depth requirements by 50%. The final outcome of this study has been to apply the design lessons learned to develop a methodology for designing a synthetic jet actuator array with the constraints of using piezoelectric-based actuator technology for flow separation control applications.
机译:本文记录了合成射流致动器阵列硬件的开发,以增强风洞模型中高升力系统的有效性。该研究涉及基于倾斜执行器配置的合成射流执行器阵列的设计,制造和基准测试,以相对于非倾斜基线模型减少体积安装要求而不会损失射流速度。包括适当的合成射流执行器系统接线和内部合成射流执行器腔压力感测,以监测执行器健康状况。从倾斜的合成射流致动器阵列获得的峰值速度为100m / s,与基线阵列(〜90m / s)相比具有优势,同时将可用深度要求降低了50%。这项研究的最终结果是应用所学到的设计经验,开发出一种设计合成射流致动器阵列的方法,并限制了将基于压电的致动器技术用于流分离控制应用的局限性。

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