Wind Tunnel
This product is an intermittent supersonic wind tunnel. The experimental air source is compressed air, featuring a compact footprint suitable for most laboratory environments. It is designed for studying the dynamic characteristics of subsonic and supersonic airflow inside a nozzle, as well as the aerodynamic characteristics of two-dimensional models under different flow conditions.
Share:
Added to cart successfully
Experimental Functions
1.Measure and study the pressure distribution inside a Laval nozzle under subsonic and supersonic flow conditions.
2.Compare theoretical pressure distribution values with experimental results.
3.When the airflow reaches supersonic conditions in the wind tunnel, compare the theoretical and measured nozzle contraction ratio (requires 32-channel pressure acquisition system).
4.Measure and study the influence of different model angles on aerodynamic pressure under two-dimensional subsonic and supersonic flow conditions.
5.Measure and study the lift coefficient of the test model under supersonic flow.
6.Observe and study the formation process and principles of shock waves and expansion waves in supersonic flow (requires optional schlieren system).
Product Attributes
|
Product Model |
F380 |
Product Name |
Intermittent Supersonic Wind Tunnel |
|
Main Materials |
Galvanized steel sheet, stainless steel, 6061 aluminum alloy |
Dimensions |
3030 × 805 × 2000 mm |
|
Product Weight |
240 kg |
Operating Environment |
Room temperature, Relative humidity ≤ 85% |
|
Input Power Supply |
Single-phase three-wire, 220V ±5%, 50Hz/60Hz |
||
|
Required Modules |
None |
Optional Modules |
Schlieren system |
Case Studies
Integrated Thermal Fluids and Energy Laboratory at Zhejiang University of Technology
Flight Demonstration Wind Tunnel at Shandong University
Multi Energy Complementary Experimental Platform at Hebei University
Statically Determinate Beam Section Internal Force Testing Apparatus Delivered to Jining Vocational and Technical College
Self Developed Compression Bar Stability and Stress Testing Apparatus Delivered to Shandong Polytechnic University
01
Integrated Thermal Fluids and Energy Laboratory at Zhejiang University of Technology
MicroNewton has equipped a five zone integrated teaching laboratory at Zhejiang University of Technology. The space covers heat transfer, thermodynamics, fluid mechanics, combustion, and multi energy systems with touchscreen stations for energy and power engineering programs.
Learn More
02
Flight Demonstration Wind Tunnel at Shandong University
MicroNewton has delivered a flight demonstration wind tunnel to Shandong University. Students operate a control stick to fly a NACA airfoil model in a subsonic flow, with a digital twin display showing lift, angle of attack, stall, and stability as they happen.
Learn More
03
Multi Energy Complementary Experimental Platform at Hebei University
MicroNewton has delivered an integrated multi energy complementary experimental platform to Hebei University of Engineering. The platform combines solar, wind, hydrogen, thermal storage, and heat pump training equipment in one source, storage, and load network for student laboratories.
Learn More
04
MicroNewton delivers self developed MST01 statically determinate beam section internal force testing apparatus to Jining Vocational and Technical College. This structural mechanics teaching equipment physically implements the section method to measure beam shear force and bending moment. It supports superposition principle verification and error analysis, suitable for civil engineering mechanical engineering and bridge related students at vocational and technical education institutions.
Learn More
05
MicroNewton self developed MS10 compression bar stability and stress testing apparatus has been delivered to Shandong Polytechnic University. This teaching device enables students to observe column buckling, measure critical load and verify Euler formula with configurable end supports. It serves civil engineering and mechanical engineering students, helping them distinguish strength failure from stability failure and compare real experimental data against theoretical material mechanics formulas.
Learn MoreRelated Products
