Coupled analysis for active control and energy harvesting from flow-induced vibration

The aerospace community has long studied active flutter control. Recently, a novel idea, which is energy harvesting from wing vibration under the assumption that certain magnitude of allowed, been attracting attention. balancing problem between piezoelectric and control an research topic. In our previous work, we developed coupled analysis system for piezoelectric–structure–fluid interaction problems. present study, integrate harvester model. With numerical examples, considered limit cycle oscillation (LCO) cantilevered beam in axial flow. Then, showed LCO suppression was achieved while scavenged by harvesters at least as much consumed