Flutter control based on ultrasonic motor for a two-dimensional airfoil section

Journal of Fluids and Structures

Volumn 28, Issue , 2012, Pages 89-102

  Yu, Mingli ^a   Hu, Haiyan ^a  

^a NANJING UNIVERSITY OF AERONAUTICS AND ASTRONAUTICS   (China)

Author keywords

Active flutter suppression; Numerical simulation; Ultrasonic motor; Wind tunnel test

Indexed keywords

ACTIVE FLUTTER SUPPRESSION; AIRFOIL SECTION; CONTROLLED SYSTEM; DYNAMIC EQUATIONS; EQUATION BASED; EXPERIMENTAL MODELING; EXPERIMENTAL STUDIES; FLOW SPEED; FLUTTER CONTROL; FLUTTER SPEED; HIGH TORQUE; LOW SPEED; LOW WEIGHT; NON-LINEAR LEAST SQUARES; PIECEWISE-LINEAR; SIMPLE APPROACH; SMALL SIZE; SUBOPTIMAL CONTROL; TORSIONAL STIFFNESS; TWO-DIMENSIONAL AIRFOILS; ULTRASONIC MOTOR; ULTRASONIC MOTORS; UNCONTROLLED SYSTEMS; WIND TUNNEL TEST; WIND TUNNEL TESTS;

AEROSERVOELASTICITY; COMPUTER SIMULATION; CONTROL SURFACES; FLUTTER (AERODYNAMICS); MOTORS; PIECEWISE LINEAR TECHNIQUES; PIEZOELECTRIC DEVICES; PIEZOELECTRIC MOTORS; TWO DIMENSIONAL; ULTRASONIC EQUIPMENT; ULTRASONIC MACHINE TOOLS; WIND STRESS; WIND TUNNELS;

AIRFOILS;

EID: 84856100911     PISSN: 08899746     EISSN: 10958622     Source Type: Journal    
DOI: 10.1016/j.jfluidstructs.2011.08.015     Document Type: Article

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