Fundamentals of Aerodynamics
This product is designed to be used in conjunction with the Basic Aerodynamics Experimental Bench and the Multi-Tube Manometer Experimental Module. It is intended for studying the flow characteristics of the boundary layer over a flat plate in aerodynamics.
The front side of the module is transparent for clear visualization. A removable and reversible partition plate is installed within the flow channel, and adjustable white lining plates at the top and bottom of the channel allow the formation of either favorable or adverse pressure gradients along the flow direction.
The device is equipped with a miniature Pitot tube, whose vertical position can be precisely adjusted using a micrometer. This enables measurement of the boundary layer thickness distribution along the flow direction.
Based on the Bernoulli equation, and using total and static pressure data measured by the multi-tube manometer, the velocity distribution within the boundary layer can be calculated.
The module also supports customization of plates with different surface roughness for extended research applications.
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Experimental Functions
1.Understand and calculate key concepts such as air density, kinematic viscosity, airflow velocity, Reynolds number, and the Bernoulli equation.
2.Study pressure and velocity distribution across the boundary layer over a smooth flat plate at different Reynolds numbers.
3.Study pressure and velocity distribution across the boundary layer over a rough flat plate at different Reynolds numbers.
Product Attributes
|
Product Model |
F103 |
Product Name |
Flat Plate Boundary Layer Experimental Module |
|
Main Materials |
Black POM, transparent acrylic, 6061 aluminum alloy |
Dimensions |
190 × 120 × 380 mm |
|
Product Weight |
2.5 kg |
Operating Environment |
Room temperature, Relative humidity ≤ 85% |
|
Input Power Supply |
None |
||
|
Required Modules |
None |
Optional Modules |
None |
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