PTW - Propeller Wind Tunnel: TEST SMARTER, FLY BETTER
Small Open Type Blower Wind Tunnel for Propellers
"A man will fly, relying not on the strength of his muscles, but on the strength of his mind"
N.E. Zhoukovsky

We are designing a compact open-circuit wind tunnel with a centrifugal blower and a wide-angle diffuser intended for propeller testing. The wind tunnel will accommodate propellers up to 20 inches (0.508 m) in diameter, achieve a maximum test-section velocity of 20 m/s (72 km/h), and operate with a 15 kW motor driving the blower at 960 RPM.

Why open blower type?

  • Cost and space efficiency: open-circuit tunnels are more economical and require less space than closed-circuit designs.

  • Avoidance of recirculation: disturbed air from the working section is not recirculated, improving flow quality for propeller testing.

  • Elimination of corners: since corners contribute significantly to pressure losses, their absence in an open-circuit design reduces energy consumption.

  • Flexible exit configuration: the exit diffuser can be omitted or adjusted for easier integration into limited spaces.

Why do we need this small tunnel?



For Fast, Precise Propeller & Powerplant Testing


Testing propellers and electric power systems in real-world conditions is time-consuming and expensive. Our wind tunnel will deliver:



Quick Comparisons – Test multiple propellers in minutes, not days.

Accurate Data – Measure thrust, efficiency, and power draw under controlled conditions.

Optimize Performance – Find the best propeller-motor combo for drones and aircraft.

Cost-Effective R&D – Avoid costly trial-and-error in the field.

How will we ensure the high quality of test data?



1. Precision Instrumentation

High-accuracy load cells (±0.1% error) for thrust/torque.
Calibrated RPM sensors and power analyzers
.
2. Flow Conditioning

4 Screens + Honeycomb – Reduces turbulence and aligns flow for uniform velocity.
Optimized porosity and positioning to minimize boundary layer effects.

3. Rigorous Calibration

Regular sensor validation against NIST-traceable standards.
Baseline tests with reference propellers.

4. Flow Quality Control

Periodic checks via pitot-static surveys and, hopefully, PIV (Particle Image Velocimetry).
Automated data filtering to eliminate electrical noise.


Result we expect? Repeatable, lab-grade data we and you can trust.

What is the expected performance of our wind tunnel?




Here are some specifications and estimated characteristics of the designed wind tunnel:



What's new?



May, 2025: we are gradually transitioning to the construction of the wind tunnel.

February, 2025: we started working on the baseline design of the wind tunnel.



karpovichea@mai.ru

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