Modeling and Test of Aerodynamic Force for a Piezoelectric Transducer Drive Mechanism

Jing Lu; Yan Fang Hang; Ying Jun Hu

doi:10.4028/www.scientific.net/AMM.631-632.610

Paper Titles

Stability Assessment of Minor-Caliber Vessel Perfusion System for Ex Vivo
p.594

Visual C++ Call MATLAB Multi-Scale Edge Detection
p.598

LSD Based Pose and Position Estimation for UAV Landing
p.602

Methods of Path Identification and Processing in Freescale Intelligence Car
p.606

Modeling and Test of Aerodynamic Force for a Piezoelectric Transducer Drive Mechanism
p.610

Design and Implementation of Service-Oriented Information Acquisition System of Smart Meter
p.614

The Research on the Tracking and Positioning Platform Based on the Android Smartphone
p.618

Stress Analysis on a Connecting Rod Big End Bearing of Two-Stroke Marine Diesel Engine
p.623

In Situ Shear Test of Zhongnan Concave Landslide
p.627

HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 631-632Modeling and Test of Aerodynamic Force for a...

Modeling and Test of Aerodynamic Force for a Piezoelectric Transducer Drive Mechanism

Abstract:

To reduce the complexity structure of a flapping rotor, a piezoelectric transducer drive mechanism is designed to achieve active flapping and passive rotary motion. Then, its aerodynamic force model is built by using Theodorsen's theory in order to analyze the aerodynamic characteristics of this system. Model simulation and experimental results show that flapping amplitude, flapping frequency and initial angle of attack make a significant role for aerodynamic characteristics. The effectiveness of aerodynamic force mode also can be seen from the comparison of the results.

You might also be interested in these eBooks

View Preview

Info:

Periodical:

Applied Mechanics and Materials (Volumes 631-632)

Pages:

610-613

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.631-632.610

Citation:

Cite this paper

Online since:

September 2014

Authors:

Jing Lu*, Yan Fang Hang, Ying Jun Hu

Keywords:

Aerodynamic Force Model, PZT Actuator, Theodorsen’s Theory

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

* - Corresponding Author

References

[1] C.P. Ellington, The novel aerodynamics of insect flight: applications to Micro-air vehicles, Journal of Experimental Biology, No. 202 (1999) pp.3439-3448.

DOI: 10.1242/jeb.202.23.3439

Google Scholar

[2] M. I. Woods, Energy requirements for the flight of Micro Aerial Vehicles, The aeronautical Journal, Volume 105, No. 1045 (2001) pp.135-149.

Google Scholar

[3] Dickinson, M. H, Gotz, K. G, Unsteady aerodynamic performance of model wings at Low Reynolds Numbers, Journal of Experimental Biology, No. 174 (1993) pp.45-64.

DOI: 10.1242/jeb.174.1.45

Google Scholar

[4] I. E. Garrick, Propulsion of a flapping and oscillating airfoil, naca-report-567(1937)2-3.

Google Scholar