NCSU Variable Mach number Supersonic Wind Tunnel
- Mach number: 1.5 to 4.0
- Test section: 6″ x 6″
- Optical accessibility
- Wall pressure measurement capability
NCSU Turbulent Jet in Vitiated Coflow Facility
- Access to conventional and distributed reaction regimes
- O2 conc. between 5% – 21%
- Center jet dia: 5 to 10 mm
- Co flow dia: 150 mm
- Jet Renolds number: 2000 – 30000
Low intensity shock tube
- Air as working medium
- Driver pressure between +15psig – 300psig
- Test duration: 10 ms