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System for global flow field management using distributed, surface-embedded, nano-scale boundary layer actuation

机译:使用分布式,表面嵌入式,纳米级边界层驱动进行全局流场管理的系统

摘要

Systems to provide distributed flow control actuation to manage the behavior of a global flow field, are provided. An example of a system can include an aerodynamic structure having an outer surface, and an array of a plurality of nano-scale effectors connected to the outer surface of the aerodynamic structure to be in fluid contact with a flowing fluid when operationally flowing, to induce controlled, globally distributed disturbances at a viscous wall sublayer of a turbulent boundary layer of the flowing fluid when operationally flowing and to manipulate fluid behavior of the flowing fluid to thereby substantially reduce pressure loss associated with incipient separation of the fluid flow from portions of the aerodynamic structure.
机译:提供了用于提供分布式流控制致动以管理全局流场的行为的系统。系统的示例可以包括具有外表面的空气动力学结构,以及连接到空气动力学结构的外表面以在操作流动时与流动流体流体接触的多个纳米尺度效应器的阵列,以诱导在操作流动时在流动流体的湍流边界层的粘性壁子层处进行受控的全局分布扰动,并控制流动流体的流体行为,从而从根本上减少与流体流与空气动力学部分的最初分离相关的压力损失结构体。

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