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Aerodynamics Engineering  Wind Tunnels
 

Revolutionize Aerodynamic Testing with Aerodynamic Engineering Wind Tunnels
 

Wind tunnels are essential tools for aerospace, automotive, and industrial research, allowing scientists and engineers to analyze airflow dynamics, lift, drag, and pressure distribution with precision. Aerodynamic Engineering’s advanced wind tunnel systems provide controlled, repeatable testing environments for studying everything from subsonic aerodynamics to supersonic shock waves. Featuring high-precision nozzle designs, real-time data acquisition, and customizable configurations, our wind tunnels deliver unparalleled accuracy and efficiency for research and development. Whether you’re optimizing aircraft performance, testing automotive aerodynamics, or conducting academic studies, Aerodynamic Engineering’s cutting-edge solutions ensure reliable, high-quality results. Take your aerodynamic testing to the next level—contact Aerodynamic Engineering today!

 

Precision,
                   Performance,
                                               and Innovation

​​Wind Tunnel Solutions

AERODYNAMIC ENGINEERING offers variable Mach number supersonic wind tunnels with test section sizes ranging from 1-inch x 1-inch (2.54 cm x 2.54 cm) to 12-inch x 12-inch (30.5 cm x 30.5 cm). These systems can be customized with compressors, dryers, and plumbing to meet a wide range of research and educational needs. Contact AERODYNE for a customized quote.

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Available Configurations

AERODYNAMIC ENGINEERING's Variable Mach Number Wind Tunnels are available in two configurations:

 

Console Configuration (For 1-inch and 2-inch systems)

A compact, self-contained laboratory requiring only compressed air. Includes:

  • Oil separator

  • Heatless desiccant air dryer

  • ASME Code storage and stagnation tanks

  • Electro-mechanical pressure control valve

  • Complete Schlieren system

  • Set of four models

  • Model positioning quadrant

  • Diffuser

 

Standard Configuration (For 3-inch to 12-inch systems)

A modular wind tunnel system, including:

  • Electro-mechanical pressure valve

  • ASME Code stagnation tank

  • Supersonic wind tunnel and diffuser

Note: Standard systems require a compressor, oil separator, dryer, storage tank, and associated plumbing, all of which can be supplied by AERODYNE.

 

Applications

  • Supersonic research

  • Educational demonstrations

 

Performance Specifications

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Nominal Mach Number Ranges

  • 1-inch & 2-inch systems: Mach 1.5 to 3.5

  • 3-inch to 12-inch systems: Mach 1.4 to 4.0

 

Advanced Data Acquisition, Display & Control

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Aerodynamic Engineering’s integrated system provides real-time data display and recording of:

  • Storage tank pressure

  • Stagnation pressure & temperature

  • Nozzle block position

  • Test section static pressure

  • (Optional) Sting force balance output

  • (Optional) Model pitch angle with motorized control

 

System Control Features

  • Stagnation pressure regulation

  • Calibrated nozzle block positioning

  • Automated Mach number set points for precision testing

Each system includes a Dell desktop computer with an executable LabVIEW file (LabVIEW software not required).

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