An Experimental Study of the Vortex Structures in the Wake of a Piezoelectric Flapping Plate for Nano Air Vehicle Applications

doi 10.31274/etd-180810-331
Full Text
Abstract

Available in full text

Date

Unknown

Authors
Publisher

Iowa State University

Related search

Onboard Stability Control System for a Flapping Wing Nano Air Vehicle

2009English

Development of Piezoelectric Actuated Mechanism for Flapping Wing Micro-Aerial Vehicle Applications

Advances in Applied Ceramics
CompositesIndustrialManufacturing EngineeringCeramics
2010English

Numerical Study of Mechanisms of the Vortex Formation in the Wake of Dual-Flapping Foils

Journal of Applied Mathematics and Physics
2017English

Large-Scale Volumetric Flow Visualization of the Unsteady Wake of a Flapping-Wing Micro Air Vehicle

Experiments in Fluids
Mechanics of MaterialsFluid FlowTransfer ProcessesComputational MechanicsAstronomyPhysics
2019English

Experimental and Computational Investigations of Flapping Wings for Nano-Air-Vehicles

Engineering Applications of Computational Fluid Mechanics
ModelingComputer ScienceSimulation
2015English

Experimental Study on Piezoelectric Energy Harvesting From Vortex-Induced Vibrations and Wake-Induced Vibrations

Journal of Sensors
ControlSystems EngineeringInstrumentationElectricalElectronic Engineering
2016English

Experimental Investigation on the Aerodynamics of a Bio-Inspired Flexible Flapping Wing Micro Air Vehicle

International Journal of Micro Air Vehicles
Aerospace Engineering
2014English

Kinematics Optimization for a Flapping-Wing Micro Air Vehicle

IFAC Proceedings Volumes
2005English

Rigid-Body Kinematics Versus Flapping Kinematics of a Flapping Wing Micro Air Vehicle

Journal of Guidance, Control, and Dynamics
ControlSystems EngineeringElectronic EngineeringApplied MathematicsSpaceElectricalPlanetary ScienceAerospace Engineering
2015English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2024 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy