Model：LSK-R52
The UAV airflow wind tunnel laboratory mainly consists of the following components: wind chamber structure, air ducting, regulating damper, support frame, pressure-measurement tube cover, and other parts. It can be customized in sizes such as 2 m × 2 m, 3 m × 3 m, 4 m × 4 m, and 5 m × 5 m. The test section size can also be tailored to customer requirements.
The UAV airflow wind tunnel laboratory mainly consists of the following components: wind chamber structure, air ducting, regulating damper, support frame, pressure-measurement tube cover, and other parts. It can be customized in sizes such as 2 m × 2 m, 3 m × 3 m, 4 m × 4 m, and 5 m × 5 m. The test section size can also be tailored to customer requirements.
Reference Standards
GB/T 1236-2017
AMCA 210-2016
The UAV airflow wind tunnel laboratory mainly includes the following sections/components: wind chamber structure, air ducts, regulating damper, supports, pressure-tapping tube cover, etc. Standard sizes such as 2 m × 2 m, 3 m × 3 m, 4 m × 4 m, and 5 m × 5 m are available, and the specific test section can be non-standard customized according to customer needs.
Specifications
| Item | Technical Specification |
|---|---|
| Structure | Carbon steel casing |
| Wind chamber size | 3 m × 3 m |
| Flow range | (5,000–50,000) m³/h |
| Pressure | ≥ 3,000 Pa |
