Integrated Sensing of Camber, Aerodynamic Load, and Vortex Structures over Membrane Wings

Abstract

Due to the compliant nature of extensible membrane wings, there exists a close relationship between the membrane wing camber and the aerodynamic load. Additionally, the membrane dynamics are often linked to unsteady large-scale flow structures, such as shear layer location or leading-edge vortex shedding. Real-time measurements of the membrane shape, including both mean camber and the frequency content of vibration, provide significant information on the surrounding flowfield. In this work, one method of integrated camber sensing is demonstrated, and the relationships to aerodynamic load and flowfield are shown. Camber is estimated via the capacitance of a dielectric elastomer membrane wing. The relationship between capacitance and camber is defined geometrically. The mean aerodynamic load is shown to be well-captured by applying a simple aeroelastic analysis to the measured camber. Finally, time-resolved membrane kinematics and flowfield measurements are used to illustrate the ties between the dynamic membrane vibration, as measured by capacitance, and the behavior of the shear layer above the wing. Ultimately, this work is a step toward an integrated, closed-loop control method for membrane wings.