F130-Low-Speed Wind Tunnel
F130-Low-Speed Wind Tunnel
F130-Low-Speed Wind Tunnel
F130-Low-Speed Wind Tunnel
F130-Low-Speed Wind Tunnel
F130-Low-Speed Wind Tunnel
F130-Low-Speed Wind Tunnel
F130-Low-Speed Wind Tunnel

F130-Low-Speed Wind Tunnel

This product is a fundamental experimental platform for low-speed aerodynamics research, designed to study basic flow principles and verify related aerodynamic theories.

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Product Description

This product is a fundamental experimental platform for low-speed aerodynamics research, designed to study basic flow principles and verify related aerodynamic theories.

 

The wind tunnel consists of the test section (including silencer), drive system, and basic control system. Various models such as airfoils, aircraft configurations, and bluff bodies can be installed in the test section to investigate aerodynamic interactions, including lift, drag, pitching moment, and pressure distribution.

 

With optional modules such as the 32-channel pressure system, smoke generator, and three-component force balance, the system supports a wide range of aerodynamic theory verification and experimental research. Some modules support customization and extended experimental design.

 

The main unit is equipped with a touchscreen display system, integrating multiple aerodynamic model interfaces. It provides real-time data visualization, dynamic curve display, and Excel data export. In addition to standard aerodynamic models, the system can also function as a versatile data acquisition platform for extended aerodynamics research.

Experimental Functions

01

Touchscreen interface with audio feedback for system control and configuration.

02

Built-in interfaces for wind tunnel model monitoring, three-component force balance display, and 32-channel pressure display, with real-time dynamic curves and Excel data export.

03

Supports full input/output control and data acquisition for all compatible modules.

04

Can serve as an extended data acquisition system for lift, drag, pitching moment, and pressure distribution measurements.

05

Study boundary layer effects and pressure distribution (requires 32-channel pressure system and boundary layer module).

06

Analyze friction drag of different bluff body shapes (requires three-component balance and 3D drag model).

07

Measure pressure distribution and lift characteristics of the NACA 0012 airfoil (requires 32-channel pressure system and airfoil model).

08

Study effects of flap deflection on lift, drag, and pitching moment of the NACA 2412 airfoil (requires force balance and airfoil module).

09

Measure aerodynamic forces on NACA 0012 wings with different spans (requires force balance and airfoil module).

10

Study lift, drag, and pitching moment characteristics of NACA 2415 high/low wing aircraft model (requires force balance and airfoil module).

11

Study aerodynamic characteristics of the S1210 airfoil model (requires force balance and airfoil module).

12

Demonstrate flow characteristics around various bluff bodies (requires smoke generator and corresponding models).

13

Conduct wake flow experiments and measure downstream pressure distribution (requires 32-channel pressure system, smoke generator, and models).

14

Provide stable, adjustable airflow for extended aerodynamics experiments.

Product Attributes

Product Model

F130

Product Name

Low-Speed Wind Tunnel

Main Materials

Galvanized steel sheet, stainless steel,

6061 aluminum alloy

Specifications

4110 × 920 × 1910 mm

Product Weight

530 kg

Operating Environment

Room temperature,

Relative humidity ≤ 85%

Input Power Supply

Three-phase five-wire system

380V ±5%, 50Hz

Required Modules

● 2 sets of Pitot tube systems
● 1 electrical control cabinet

Optional Modules

● 32-channel pressure acquisition system
● Three-component force balance
● 3D drag model
● Flat plate boundary layer model
● NACA 0012 airfoil model
● High/low wing aircraft model
● Airfoil model kit
● Smoke generator

FAQ

Is your company a manufacturer or a trading company?

We are a direct source manufacturer with independent R&D, production and quality inspection workshops, and have years of expertise in the university laboratory equipment sector.

What payment methods are supported for overseas orders?

We accept T/T (Telegraphic Transfer) and irrevocable sight L/C (Letter of Credit). Formal commercial or proforma invoices are issued for all orders, with a transparent and traceable process.

What is the production and delivery cycle for the equipment?

Standard models: 45-60 days. Expedited production is available for urgent orders with priority scheduling, and the exact lead time is negotiable.

Do you support product customization?

Customization, OEM and ODM services are available. We can adjust parameters, structure, size and functions as required, and accept private labeling production.

How do you ensure the safe transport of the equipment?

Export-grade triple shockproof and moisture-proof packaging (shockproof foam + thickened carton + plywood wooden case) with warning labels attached. 

Does the product come with a warranty? Are spare parts included?

All products come with a 2-year free original factory warranty, and common wearing parts are provided free of charge during the warranty period.
Overseas After-Sales Support:
• 7×24h remote technical support and free operation training with one-on-one engineer guidance;
• Free urgent air shipment of replacement parts for non-human-induced quality defects within the warranty period;
• Lifetime technical consultation and cost-price spare parts supply after warranty;
• Bilingual manuals, operation videos and experiment guides are included for easy use by beginners.

How do you control product quality before shipment?

Strict three-level quality inspection is carried out before delivery:
1. Raw Material Inspection: Full inspection of core components to control precision;
2. In-Process Inspection: Special personnel monitor each process to avoid defects;
3. Final Shipment Inspection: Power-on testing and precision calibration, with official inspection reports issued; factory inspection and remote inspection are both supported.

Case Studies

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In 2026, a new batch of compressed air energy storage teaching experimental equipment was successfully delivered, empowering universities with micro-newton technology for new energy teaching

01

In 2026, a new batch of compressed air energy storage teaching experimental equipment was successfully delivered, empowering universities with micro-newton technology for new energy teaching

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