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LW-6200 Wind Tunnel
Specifications
1. Open-loop suction type wind tunnel structure
2. Test section dimension: 0.2 (W) × 0.2 (H) × 0.8 (L) m
3. Flow field quality:
3.1. Met over 80% of the cross-section area from axial center at 2 m/sec or up
3.2. Uniformity >98%
3.3. Turbulence intensity <0.5%
4. Speed range: 0.5 ~ 25 m/sec
5. Wind tunnel dimension: 0.7 (W) × 3.2 (L) × 1.8 (H) m (Ref.)
6. Space required: 1.5 (W) × 4.5 (L) × 2.5 (H) m (Ref.)
7. Power source: AC220V, 3 phases, 10 Amp
8. Weight: 400 kg (Ref.)
Experiments
1. Static pressure, total pressure and speed measurement
1.1. By Pitot static pressure probe,
1.2. Differential pressure meter, 0~127.0 mmAq, and accuracy <0.25%
1.3. TSI hot wire anemometer
2. Flow deflection measurement
3. Lift and drag force measurement
4. Pressure distribution
5. Boundary layer experiment
6. 2D/3D flow visualization
1. Open-loop suction type wind tunnel structure
2. Test section dimension: 0.2 (W) × 0.2 (H) × 0.8 (L) m
3. Flow field quality:
3.1. Met over 80% of the cross-section area from axial center at 2 m/sec or up
3.2. Uniformity >98%
3.3. Turbulence intensity <0.5%
4. Speed range: 0.5 ~ 25 m/sec
5. Wind tunnel dimension: 0.7 (W) × 3.2 (L) × 1.8 (H) m (Ref.)
6. Space required: 1.5 (W) × 4.5 (L) × 2.5 (H) m (Ref.)
7. Power source: AC220V, 3 phases, 10 Amp
8. Weight: 400 kg (Ref.)
Experiments
1. Static pressure, total pressure and speed measurement
1.1. By Pitot static pressure probe,
1.2. Differential pressure meter, 0~127.0 mmAq, and accuracy <0.25%
1.3. TSI hot wire anemometer
2. Flow deflection measurement
3. Lift and drag force measurement
4. Pressure distribution
5. Boundary layer experiment
6. 2D/3D flow visualization
PC-based data acquisition system and hot wire anemometer