Piezoaeroelastic modeling and analysis of a generator wing with continuous and segmented electrodes

Journal of Intelligent Material Systems and Structures

Volumn 21, Issue 10, 2010, Pages 983-993

  De Marqui Jr , Carlos ^a   Erturk, Alper ^b   Inman, Daniel J ^b  

^a UNIVERSITY OF SÃO PAULO   (Brazil)

^b Virginia Polytechnic Institute and State University   (United States)

Author keywords

aeroelasticity; electrode configuration; energy harvesting; piezoaeroelasticity; piezoceramics; unmanned air vehicles.

Indexed keywords

AEROELASTIC MODES; AEROELASTIC VIBRATION; AIRFLOW SPEED; APPLICATION PLATFORMS; BROADBAND PERFORMANCE; COUPLED BENDING; COUPLED MODE; ELECTRICAL ENERGY; ELECTRICAL OUTPUT; ELECTRICAL POWER; ELECTRICAL POWER OUTPUT; ELECTRODE CONFIGURATION; ELECTRODE CONFIGURATIONS; ELECTRONIC COMPONENT; ENERGY SOURCE; FINITE ELEMENT MODELS; FLUTTER SPEED; LIFTING SURFACES; MODELING AND ANALYSIS; PIEZO-CERAMICS; PIEZOELECTRIC POWER; SEGMENTED ELECTRODES; SHUNT DAMPING; TORSIONAL MOTION; UNMANNED AIR VEHICLES; UNSTEADY AERODYNAMICS; VIBRATION-BASED ENERGY HARVESTING;

AERODYNAMICS; AEROELASTICITY; ELASTIC WAVES; ELECTRIC POWER SUPPLIES TO APPARATUS; ELECTRODES; ENERGY HARVESTING; FINITE ELEMENT METHOD; FLEXIBLE WINGS; HARVESTING; MICRO AIR VEHICLE (MAV); REMOTELY OPERATED VEHICLES; SPEED; UNMANNED AERIAL VEHICLES (UAV); VEHICLES;

ELECTRIC GENERATORS;

EID: 77954339620     PISSN: 1045389X     EISSN: 15308138     Source Type: Journal    
DOI: 10.1177/1045389X10372261     Document Type: Article

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