Correlation of Structural Strain to Tip Vorticity and Lift for a MAV Pliant Membrane Wing
作者： Trenton Carpenter , Cody Ray , Roberto Albertani
DOI: 10.1007/978-1-4614-4226-4_1
关键词: Vorticity 、 Membrane wing 、 Wind tunnel 、 Wing 、 Lift (force) 、 Improved performance 、 Aerospace engineering 、 Computer science 、 Micro air vehicle 、 Aerodynamics
摘要: The last decade has witnessed a surge of scientific interest in flight at the micro air vehicle (MAV) scale. To date, MAV utilizing an adaptable, flexible smart wing design yet to come fruition. While highly aerodynamic surfaces have repeatedly demonstrated improved performance through passive adaptation, limited structural and flow state knowledge prevents inclusion active control strategies which could improve such designs.
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