Aerodynamic experimental parameters automatic acquisition technology

Author

Qiao, Xiangxin ; Yao, Jun ; Jian, Maosheng ; Liu, Zhihe

Author_Institution

Dept. of Sch. Equip., Shenyang LiGong Univ., Shenyang, China

fYear

2011

fDate

21-23 June 2011

Firstpage

1434

Lastpage

1437

Abstract

Introduces the basic structure of MAF wind tunnel, technical parameters, testing principle, six component balance installation and the principles of the experiment, design and hardware composition of the data acquisition system, aerodynamic calculation, software interface design. Test model is an example of a projectile aerodynamic wind tunnel testing and experimental results with a FD-04 wind tunnel of comparison, show that the experimental methods and testing technology can be used for practical engineering applications.

Keywords

aerodynamics; data acquisition; mechanical engineering computing; user interfaces; wind tunnels; FD-04 wind tunnel; MAF wind tunnel; aerodynamic experimental parameters automatic acquisition technology; component balance installation; data acquisition system; projectile aerodynamic wind tunnel testing; software interface design; Aerodynamics; Computational modeling; Data acquisition; Data models; Force; Software; Testing; aerodynamic; balanc; data acquisition; wind tunnel;

fLanguage

English

Publisher

ieee

Conference_Titel

Industrial Electronics and Applications (ICIEA), 2011 6th IEEE Conference on

Conference_Location

Beijing

ISSN

pending

Print_ISBN

978-1-4244-8754-7

Electronic_ISBN

pending

Type

conf

DOI

10.1109/ICIEA.2011.5975814

Filename

5975814