Fundamentals of Aerodynamics
This product is designed to be used together with the Air Dynamics Basic Experimental Platform (F100) and the multi-tube manometer module (F101). It is used for experimental research on the aerodynamic characteristics of airfoil flow under low-speed conditions.
The module consists of a visual rectangular flow channel with a fixed symmetric airfoil installed inside. Pressure measuring points are evenly distributed along the chordwise direction on the airfoil surface. When connected to the multi-tube manometer, the pressure at each point can be measured to plot the pressure distribution curve.
The module also allows precise adjustment of the airfoil angle of attack during experiments.
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Experimental Functions
1.Study the surface pressure distribution of an airfoil under low-speed flow conditions.
2.Understand the geometric parameters and aerodynamic parameter definitions of an airfoil.
3.Study and experimentally analyze airfoil lift-line theory.
4.Measure lift and plot the lift curve.
Product Attributes
|
Product Model |
F111 |
Product Name |
Airfoil Pressure Distribution Experimental Module |
|
Main Materials |
Black POM, transparent acrylic, white photosensitive resin |
Dimensions |
308 × 120 × 261 mm |
|
Product Weight |
1.6 kg |
Operating Environment |
Room temperature, Relative humidity ≤ 85% |
|
Input Power Supply |
None |
||
|
Required Modules |
Pressure tubing (10 m) |
Optional Modules |
None |
Case Studies
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