Aerodynamic experimental parameters automatic acquisition technology

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.