Analysis of the Bionic Wing's Aerodynamic Performance

Jing Shan Jiao; Xin Hua; Zhang Ji

doi:10.4028/www.scientific.net/AMM.644-650.385

Paper Titles

Adaptive Stable Control for Chaos Systems by New Fuzzy Inference Systems without Any Rule Base
p.367

Numerical Simulation on Air Volume Flow Rate Distribution of Stator Ducts for Salient Pole Synchronous Motor
p.373

Experimental Study of Flow Field of Large Air-Cooled Turbine Generator for Multi-Ventilation Ducts of Stator
p.377

Design of the Automatic Guided Vehicle Control System Applied to Automotive Logistics
p.381

Analysis of the Bionic Wing's Aerodynamic Performance
p.385

Flow Induced Vibration in the Seal System
p.390

Simulation for the Combustion System Work Process in Internal Combustion Engine
p.394

Dynamic Analysis of Large-Displacement Motion Simulator
p.398

Finite Element Simulation of Track Shoe and Ground Adhesion
p.402

HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 644-650Analysis of the Bionic Wing's Aerodynamic...

Analysis of the Bionic Wing's Aerodynamic Performance

Abstract:

According to a certain type of flying in the no imitation gull wing design straight wing with man. Then the bionic wing and conventional airfoil are simulated, and compared the two kinds of wing aerodynamic parameters. The study found, hale no flow man-machine bionic wing design can effectively improve the wing, reduce the upper wing surface flow separation, reduce the lift loss, reduce the pressure drag, improve the lift drag ratio of the wings. In this paper, the simulation results for the design of the UAV wing provides certain reference.

You might also be interested in these eBooks

View Preview

Info:

Periodical:

Applied Mechanics and Materials (Volumes 644-650)

Pages:

385-389

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.644-650.385

Citation:

Cite this paper

Online since:

September 2014

Authors:

Jing Shan Jiao*, Xin Hua, Zhang Ji

Keywords:

Bionic Wing, Numerical Simulation

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

* - Corresponding Author

References

[1] Chen Zhiliang. Air dynamics (M). Beijing: Beijing University of Aeronautics and Astronautics Press, (2009).

Google Scholar

[2] Li Weijie. [D]. simulation of bionic wing by Jilin University resistance value, (2009).

Google Scholar

[3] Hua Xin. Numerical Simulation And Aerodynamic Performance Comparison Between Seagull Aerofoil and NACA 4412 Aerofoil under Low-Reynolds[J]. Advances in Natural Science, 2010, 3(2): 244-250.

Google Scholar

[4] Hua Xin. High Altitide and Long Endurance Unmaned Aerial Vehicle Bionic Airfoil Research.

Google Scholar

[5] Hua Xin. Base on imitation seagullairfoil UVA wing numerical simulation[J]2012, 3(1)323-325.

Google Scholar