Mach-6 Hypersonic Ludweig Tube tunnel
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Specifications
Major Functions / Key Features
The tunnel generates a Mach-6 hypersonic flow for the experimental investigation of the physics and mechanisms of hypersonic flows.
- Equipped with the Schlieren system, Rayleigh scattering system, Infrared thermography technique, pressure-sensitive paint, temperature-sensitive paint, and PCB/Kulite pressure sensors.
- Research topics include boundary layer transition process, flow control, etc.
Location
GH034Restriction
- Only for trained user
- Required project approval
Fee
On enquiry basis (sample dependent)Other Information
Manufacturer: Batou Wentian Keji Company
Model:
Category: Engineering
Owned by: Department of Aeronautical and Aviation Engineering
Contacts
Prof. Wen Chih-yung
Department of Aeronautical and Aviation Engineering
- 34002522
- cywen@polyu.edu.hk
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