Product Introduction：
This product is an intermittent supersonic wind tunnel with compressed air as the experimental gas source. It occupies a small area and can be used for experimental research in general laboratories. A wind tunnel used to study the dynamic characteristics of subsonic and supersonic airflow inside a nozzle, as well as the aerodynamic characteristics of a two-dimensional airflow model.
detailed information
| PRODUCT MODEL | F380 | product name | Intermittent Supersonic Wind Tunnel |
| Product specifications | 3030mm×805mm×2000mm | 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、Measure and study the pressure distribution inside the Laval nozzle during subsonic/supersonic flow; 2、Based on the previous experimental results, compare and analyze the difference between the theoretical and measured values of pressure distribution; 3、When the airflow in the wind tunnel reaches supersonic speed, compare and analyze the theoretical and measured values of the contraction ratio of the Laval nozzle (requiring a 32 channel pressure acquisition instrument); 4、Measure and study the effect of different model angles on the aerodynamic pressure acting on the model in two-dimensional subsonic/supersonic flow states; 5、Measure and study the lift coefficient of the test model in supersonic flow; 6、Observe and study the processes and principles of shock and expansion waves generated in supersonic flow (requiring a jet sheath schlieren system); |