Product Introduction：
This product is widely used as a fundamental experimental platform for studying the basic laws of low-speed aerodynamics, verifying and developing related theories; A wind tunnel is mainly composed of a tunnel body, a drive system, and a measurement and control system. The test section can install various wing shapes, aircraft, and other object models to study the interaction between air and the model, including lift, drag, pitch moment, pressure distribution, etc; By combining variable frequency speed regulation, 32 channel pressure testing unit, smoke generator, and three component balance module, multiple aerodynamic related experimental research and theoretical verification can be carried out. Some module models support customized expansion, experimental design, and expansion;
detailed information
| PRODUCT MODEL | F130 | product name | Low-Speed Wind Tunnel |
| Product specifications | 3550mm in length, 1100mm in width, and 1850mm in height | product material | alloy |
| Usage environment | Room temperature, relative humidity ≤ 85% | Input power supply | Single three wire, 220V, 50HZ |
| Belonging series | aerodynamics | Cooperate with modules |
| Experimental function： |
| 1、Can be used to test the characteristics of airflow pressure distribution and lift around the NACA0012 symmetrical wing; 2、Can be used to study the effects of NACA2412 flap deflection on lift, drag, and pitch moment; 3、Can be used to study the measurement of lift, drag, and pitch moment of NACA0012 on two wings of different lengths; 4、Can be used to study the lift, drag, and pitch moment laws of the NACA2415 low high wing aircraft model; 5、Can be used to study the lift, drag, and pitch moment laws of the S1210 asymmetric wing model; 6、Can be used to demonstrate the distribution of fluid flow characteristics around various shapes (in conjunction with smoke generators); 7、Can be used to conduct wake experiments and calculate the pressure distribution in the downwind direction of the model (in conjunction with a smoke generator); 8、Can be used for related extended experiments to provide a stable and variable flow velocity airflow field; |