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 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?
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?
February, 2025: we started working on the baseline design of the wind tunnel.
karpovichea@mai.ru