Aerodynamic Performance Testing Machine DC Low-Speed Wind Tunnel

• Customization: Available
• After-sales Service: Lifetime Service
• Warranty: 1year
• Model NO.: HJ
• Test Section Wind Speed Range: (0.3-32)M/S
• Cross-Sectional Dimensions: 320mm*320mm
• Flow Velocity Uniformity Coefficient: ≤1%(1-32m/S);±0.02m/S(0.3-1m/S)
• Wind Tunnel Form: DC Low-Speed Wind Tunnel
• Transport Package: Wooden Box Package
• Specification: 600 (W) x 460 (D) x 380 (H) mm
• Trademark: Hongjin
• Origin: China

Product Description

Product Description

Application scope:

The DC low-speed wind tunnel is suitable for the study of aerodynamic performance of aerospace
vehicles, especially the study of performance 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 DC low-speed wind tunnel also includes the aerodynamic characteristics of wind power machinery, the stress state of single or group building structures in the wind field and their response characteristics to wind loads, as well as the wind load state and wind vibration laws 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

DC low-speed wind tunnel:
Small footprint
Low investment
Simple control
Can perform smoke flow experiments

Product Parameters

Project	Parameters
Wind tunnel form	DC low-speed wind tunnel
Contraction section outlet cross-sectional dimensions	320mm×320mm
Test section air velocity range	(0.3~32)m/s
Flow velocity stability coefficient	≤0.5%(1~32m/s);±0.02m/s(0.3~1m/s)
Flow velocity uniformity coefficient	≤1%(1~32m/s);±0.02m/s(0.3~1m/s)
Turbulence degree	≤0.5%(≥1m)
Test section dimensions	320*320, length 800mm

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