Supersonic Wind Tunnel

Specification:

Supersonic Wind Tunnel Of 2.5 Mach With Schilieren Apparatus And Data Acquisition

• Silencer will be connected to the other end of test section. Pressure tappings will be taken in the pipe line with 2 pressure gauges for calculation of Mach number.
• of pressure sensors in the flow path – 5 Nos. with 1 No. pressure indicator
• Nozzle of 5.9mm throat × 40mm width which is made of Aluminum alloy material. Develops 2.5 Mach
• Test section of 32.5mm × 40mm × 90mm having 2 side transparent acrylic sheet of 25mm thick removable with model holding chamber.
• The testing time will be 35secs. (Approximate).
• The Schilieren mirrors will be mounted across the test section.
• 120mm mirror & 800mm focal length with illuminated point source light and knife edge stand.
• The digital camera will be provided
• Platform to record and measure the system • Tripods for 2 mirrors, 1 for illumination lamp, and 1 for camera will be provided.
• Control panel to suit for computer, computer hardware, printer, and volt stab other Mach Number  and  test section size modified as per requirements