Development of piezoelectric actuators for active flow control

被引:54
作者
Cattafesta, LN [1 ]
Garg, S [1 ]
Shukla, D [1 ]
机构
[1] High Technol Corp, Hampton, VA 23666 USA
关键词
D O I
10.2514/2.1481
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The development of piezoelectric actuators for active flow control is discussed. The type of actuators considered consists of a single sheet of piezoceramic material bonded to the underside of a shim: a "unimorph" flap design. Existing theoretical beam models are extended to incorporate a linear strain distribution in the composite unimorph beam structure. This model is combined with an optimization scheme to design a flap that maximizes the tip deflection per unit voltage for a given bandwidth. The optimization model is then used to design a piezoelectric actuator. The model predictions compare favorably to measurements of the actuator frequency response function. A sample application to control of separated flow from a backward-facing step is also described, in which the actuator is installed at the origin of the free shear layer. Detailed hot-wire measurements, together with dimensional analysis, reveal the physical mechanism responsible For the fluid-structure coupling. A quasi-static model based on the solid-body displacement of the incoming shear layer accurately describes the peak streamwise velocity perturbations produced by the actuator. This model leads to a proportional relationship between the flap tip displacement, the incoming boundary-layer profile parameters, and the streamwise velocity fluctuations produced by the actuator.
引用
收藏
页码:1562 / 1568
页数:7
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