Product Introduction：
This product is used in conjunction with an aerodynamics basic experimental platform and a multi tube pressure gauge to conduct experimental research on the aerodynamic characteristics of low-speed airfoil flow in aerodynamics. The main body is a visualized rectangular flow channel, with a NACA2412 symmetrical wing fixedly installed. Pressure measuring points are uniformly distributed at various chordwise positions on the surface of the wing, and multiple tube pressure gauges are used to measure the pressure at each point and draw pressure distribution maps; The module can accurately adjust the wing rotation angle during the experiment. Support wing customization and expansion.
detailed information
| PRODUCT MODEL | F111 | product name | Airfoil Pressure Distribution Experiment Module |
| Product specifications | Length 120mm/Width 208mm/Height 261mm | product material | alloy |
| Usage environment | 0 ℃ ≤ temperature ≤ 45 ℃, relative humidity ≤ 85 | Input power supply | not have |
| Belonging series | aerodynamics | Cooperate with modules | F100 |
| Experimental function： |
| 1、Can be used to study the surface pressure distribution of airfoils flowing at low speeds; 2、Can be used to understand the geometric and aerodynamic parameter definitions of wings; 3、Can be used to understand and study the theory of wing lift lines and conduct experimental analysis; |