Title :
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
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;
Conference_Titel :
Industrial Electronics and Applications (ICIEA), 2011 6th IEEE Conference on
Conference_Location :
Beijing
Print_ISBN :
978-1-4244-8754-7
Electronic_ISBN :
pending
DOI :
10.1109/ICIEA.2011.5975814
