Educational Wind Tunnel (EWT) System

Complete Educational Wind Tunnel (EWT) System
The AEROLAB Educational Wind Tunnel (EWT) System is a powerful tool for educators and researchers, alike. With many optional features available, the budget-conscious user can start with a basic system and upgrade as needs change or funding becomes available. The Complete EWT System is an easy-to-use, all-in-one fluids / aerodynamics laboratory. Optional features include instrumentation, data acquisition, models and probes. Contact AEROLAB and build a system today!

Click here for a downloadable brochure
Perfectly scaled for high school or university use, the basic EWT system is also popular with small technical businesses needing an accurate, reliable testing device.
Common Applications:
Education, research, testing, calibration
Performance Specifications:
- Airspeed Range - 10 mph (4.5 m/s) to 145+ mph (65 + m/s)
- Turbulence Level - less than 0.2%
- Reynolds Number (per foot) - 1.4 x 10^6 /foot
Detailed Description:
- Test Section Dimensions - 12”x12”x24” (30.5cm x 30.5cm x 61cm)
- Length - 15 feet (4.6m)
- Width - 42 inches (1.1m)
- Height - 6 feet (1.8m)
- Weight - approximately 600 pounds (272 kg)
- Power - 10 hp (7.5 KW) electric motor
- Mobility - Four (4) industrial-grade steel casters with polyurethane wheels
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EWT Test Section |
- Fiberglass Construction - Accurately-formed, rugged, and strong
- Honeycomb Flow Straightener - Expanded aluminum, 4-inch deep hexagonal cells
- Turbulence-reducing Screens - Two (2) 20x20 (mesh) stainless steel screens
- Contraction Contour - 9.5:1 propietary contraction
- Static Pressure Ring - Non-invasive access to test section static pressure used for airspeed indication
- Test Section - Anodized aluminum structure with integrated yaw table
- Visibility - Two (2) top-hinged Acrylic side doors and one (1) top window
- Diffuser - 6-deg included divergence angle with an expansion ratio of 1:3
- Motor Control - Variable Frequency Drive (VFD), configurable to all international Voltages
- Noise Attenuator - Integrated double-walled construction
Optional Features:
Data Acquisition, Display and Control (DAC) System
- National Instruments hardware and LabVIEW software (no license necessary)
- Capable of monitoring: Force/Moment Balance output, pressures, model angle of attack, and temperature (additional hardware required)
- Capable of setting and maintaining wind tunnel airspeed (dynamic pressure) regardless of model orientation
- Dell desktop computer with required peripherals included
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3-Component Force/Moment Sting Balance
- Simultaneously measure Normal Force, Axial Force, and Pitching Moment
- Quickly reconfigurable to measure Side Force, Axial Force, and Yawing Moment
- 3/8-inch outside diameter sting mount
- Adaptable to alternate model positioning systems
- 1st-order Factory calibration (supplied with Balance-specific calibration bar)
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Model Positioning System (MPS)
- Designed specifically for the EWT (but adaptable to other test sections)
- Parallelogram design keeps models centered regardless of pitch angle
- Manually operated (gearbox) pitch control +/- 20-deg
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Drag Model Set
- Mountable to a 3/8-inch sting
- Five (5) model set
- teardrop
- backward cup
- sphere
- forward cup
- circular flat plate
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1:48 th Scale F-16 Model
- 11.5 inches (29.2cm) long with 7.5 inch (19cm) span
- Mountable to a 3/8-inch Sting
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Wing with Slat and Flap
- Clark Y-14 airfoil
- Adjustable slat and flaps
- Mountable to a 3/8-inch Sting
- 9.875 inch (25cm) span and 3.5 inch (9cm) chord
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Pressure Cylinder
- 24 flush-mounted pressure taps along its circumference
- Angular position is manually set from the yaw table (vertical mount)
- Outside diameter of 4 inches (10.2cm)
- Supplied with all necessary tubing
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Pressure Wing
- 18 flush-mounted pressure taps around the Clark Y-14 airfoil
- Angular position is manually set from the yaw table (vertical mount)
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Boundary Layer Plate and “Mouse”
- 10-tap total pressure probe (“mouse”)
- Three streamwise mouse stations along the length of the flat plate
- Pressure taps ascend at an angle to span the boundary layer
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Wake "Rake"
- 18 total-pressure ports
- Ports span ~1.75 inches (4.445cm)
- Probe Length ~10 inches (25.4cm)
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Yaw Probe

- Three pressure ports with 60-deg spacing
- Overall length of 10.5 inches (26.7cm), outside diameter of 0.125 inches (32mm)
- Mounts easily in EWT test section window probe port
- Adjustable triangular base for angle indication
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Pitot-static Probe

- Rounded tip total-pressure port and 6 static ports
- Mounts easily into the test section window
- Reaches 2.6 inches (6.6cm) forward of the bend and extends 13 inches (33cm) to the bend witn an outside diameter of 0.125 inches (32mm)
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Turbulence Sphere
- Highly polished
- 4 inch (10.2cm) diameter
- Mountable to a 3/8-inch sting
- Critical Reynolds number determination with balance data only - sphere has no pressure ports
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Multi-columnn Manometer
- 24-tube
- 0 – 14 inches (0 – 35cm) of water
- Anodized alumnimum, glass tubes, brass fittings and silicone tubing
- Silk screen scale and grid
- Mounts to the EWT
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Model Storage and Display Cabinet
- Plexiglas top-hinged door with aluminum handle
- Convenient storage for models, tools and documentation
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Smoke Generator
- Electrically operated
- Produces think white smoke for flow visualization
- Includes one gallon (3.79 liters) of smoke fluid
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Pressure Transducer Array
- High-accuracy solid-state absolute pressure transducers available in 12,18 and 24-Channel blocks
- RS 485 communication simplifies and reduces wiring
- Anodized aluminum housing
- Directly integrates with the EWT DAC or as a stand-alone unit (USB interface)
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Pressure Spheres (Turbulence)
- Set of 4 Spheres
- EWT model positioning system mount provided
- One (1) total port and one (1) static port (averaged from four (4) 22.5-deg static ports)
- Storage case included
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3/8-inch "Dummy" Sting
- A low-risk alternative for mounting visualization or pressure models
- Identical dimensions to the 3/8-inch sting
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Related Products:
AEROLAB has been designing and building custom open circuit and closed circuit wind tunnels for decades.
If an EWT can’t fill your needs exactly, contact AEROLAB with a set of specifications. A custom wind tunnel system can be designed and a formal quotation will be offered.
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