Fluid Structure Interaction Simulation on the Bionic Airfoil of the Small Unmanned Plane

Zeng Qiang Qiao; Yong Bo Yang

doi:10.4028/www.scientific.net/AMM.387.241

Paper Titles

Fatigue Damage Research on Rod-Fastening Rotor of Gas Turbine Considering Start-Up Stage
p.221

The Abrasive Resistance Study about the Cutting Picker 40Cr of Coal Cutter
p.227

Study on Microstructure and Properties of Plasma Arc Surfacing Layer for Cutting Pick
p.231

Design and Development of Folded Table Bicycle Based on Solid Edge and ANSYS
p.237

Fluid Structure Interaction Simulation on the Bionic Airfoil of the Small Unmanned Plane
p.241

The Civil Airports Machinery and Equipment Innovative Design Preferred
p.246

Design of the Sled Motor Based on the Bionics
p.250

Study on Direct Current Controlled Distribution Static Synchronous Compensator with Mechanical Properties Used for Improvement of Voltage Quality
p.254

The Track-Controlling System for Mobile Greenhouse Robots
p.258

HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 387Fluid Structure Interaction Simulation on the...

Fluid Structure Interaction Simulation on the Bionic Airfoil of the Small Unmanned Plane

Abstract:

The quality and dependability of the small unmanned plane is more and more important currently. For the small unmanned plane under the conditions of Low-Reynolds, the air viscosity has relatively greater influence on its aerodynamic performance. This is one of the greatest difficulties to design a small unmanned plane. The aerodynamic performance of bionic aerofoil and NACA 4412 is contrastively analyzed while the Reynolds-Number is and by the Fluent. The computational result and the analysis show that the fluid-structure interaction is an important issue to consider while designing the small unmanned plane.

You might also be interested in these eBooks

Applied Mechanics, Materials and Mechanical Engineering

View Preview

Info:

Periodical:

Applied Mechanics and Materials (Volume 387)

Pages:

241-245

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.387.241

Citation:

Cite this paper

Online since:

August 2013

Authors:

Zeng Qiang Qiao, Yong Bo Yang

Keywords:

Aerodynamic Characteristics, Aerofoil, Low-Reynolds, Unmanned Plane

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

References

[1] Stew Magnuson, FAA Sets Date for Small Unmanned Planes in U.S. Airspace , http: /www. nationaldefensemagazine. org/archive/2011/October/Pages/FAASetsDateforSmallUnmannedPlanesinUSAirspace. aspx , 2011. 10.

Google Scholar

[2] Michael S. Selig, James J. Guglielmo, Andy P. Broeren, ＂Experiments on Airfoils at Low Reynolds Number(Translation Journals style)＂[J], AIAA-1996-62, 34th Aerospace Science Meeting and Exhibit, NV, Jan1996, pp.15-18.

DOI: 10.2514/6.1996-62

Google Scholar

[3] Tianshu Liu, K. uykendoll, R. Rhew, S. Jones，Avian Wings [J]. AIAA 2004-2186.

Google Scholar

[4] Franck Bertagmolio, Niels Sorensen. Wind turbine airfoil catalogue[J]. Pitney management services Denmark A/S. (2001).

Google Scholar

[5] Hong-li Li，Design and Investigation of Aerodynamic Performance of dedicated Airfoil Families for Horizontal-Axis Wind Turbines [D], Graduate School of Chinese Academy of Sciences , 2009. 5.

Google Scholar

[6] MUELLER T.J. ＂The Influence of Laminar Separation and Transition on Low Reynolds Number Airfoil Hysterics (Translation Journals style)＂[J], Journal of Aircraft, vol22, 1985, pp.764-770.

DOI: 10.2514/3.45199

Google Scholar

[7] Rong Ma, Peiqing Liu. Simulation of Low-Reynolds-Number and High-Lift Airfoil S1223 [J]，Proceedings of the World Congress on Engineering 2009 Vol II，July 1-3, (2009).

Google Scholar