Double Test Section Direct-Flow Low-Speed Wind Tunnel Aerospace Vehicles Testing Machine

• Customization: Available
• After-sales Service: Lifetime Service
• Warranty: 1year
• Model NO.: HJ
• Wind Tunnel Structure: DC Type
• Noise: <80dB
• Motor Power: 5kw
• Stability of Airflow: ≤0.5%
• Transport Package: Wooden Box Package
• Specification: 600 (W) x 460 (D) x 380 (H) mm
• Trademark: Hongjin
• Origin: China

Product Description

Application scope: 
The Direct-flow low-speed wind tunnel is suitable for the study of aerodynamic performance of aerospace vehicles, especially the performance study during takeoff and landing. In addition, it is also used to study the fluid dynamic performance of underwater weapons and the aerodynamic characteristics of aerospace life-saving equipment, as well as the aerodynamic performance of cars and trains. The research scope of the Direct flow low speed wind tunnel also includes the aerodynamic characteristics of wind power machinery, the stress state of single or group buildings in the wind field and their response characteristics to wind loads, as well as the wind load state and wind vibration law of bridges. These studies are not only crucial to aerospace engineering, but also play an indispensable role in transportation, housing construction, wind energy utilization and other fields.

 

Features

1. Small footprint
2. Low investment
3. Simple control
4. Can be used for smoke flow experiments
5. Stable low wind speed measurement

Product Parameters

Wind tunnel structure	DC type
Test section velocity range	First test section: (0.1-2)m/s
	Second test section: (2-35)m/s
Closed double test section dimensions	First test section: 500mmx500mm
	Second test section: 150mmx150mm
Uniformity of airflow in the working section	≤1%
Stability of airflow in the working section	≤0.5%
Noise	<80dB
Motor power	5kw
Test environment conditions	(15~30)ºC
	≤80%RH
Dimensions	8920mmx2000mmx2000mm

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