Transonic Cart – Precision Testing for Aerodynamic Performance
Advanced Testing Solutions by Syntelli
The Low Speed Wind Tunnel is designed for aerodynamic experimental testing at low speeds, particularly for applications such as aircraft embarkation processes and store separation tests using Captive Trajectory System (CTS) equipment. This system allows for accurate testing of aircraft and payloads under controlled, low-speed airflow conditions, essential for optimizing aircraft design and performance.
Ideal for researchers and engineers working on aircraft testing and payload separation, the Low Speed Wind Tunnel provides reliable results in a variety of aerospace applications.
Key Specifications
- Type: Horizontal Göttingen type
- Nozzle Outlet: Equilateral octagonal shape (opposite side distance: 2.5 meters)
- Max. Air Speed: 70 m/s
- Application: Aircraft embarkation testing, store separation, and CTS testing
Syntelli's Expertise in Testing
- Tailored solutions for low-speed aerodynamic testing
- Accurate testing environments for aircraft and payload separation
- Support for aerospace research and development in the United Arab Emirates
Contact Us for more information on how our Low Speed Wind Tunnel can support your testing needs. Reach out to our Sales and Service Department or complete the Inquiry Form for tailored solutions.