AERODYNAMICS LABORATORY
Subsonic Wind Tunnel Facility
Test section: 0.6m x 0.6m x 2m;
Max Speed: 30m/s
Instruments: PIV, Hot-wire Anemometer, Pressure Scanner, F/T Sensor, Pressure probes, Micromanometers, Smoke generator
Shock Tube
Driver Tube Length: 0.4m
Internal Diameter: 0.029m
Driven Tube Length: 0.6m
Diaphragm material: Tracing paper (90-95 gsm) Diaphragm
Table top Hypersonic Shock Tunnel Facility
Test section: 0.17m x 0.17m x 0.2m;
Mach No.: 6
Instruments: Schlieren, Shadowgraph, High Speed Camera, Pressure transducer, Accelerometer, Digital Oscilloscope.
Mach No.: 6
Instruments: Schlieren, Shadowgraph, High Speed Camera, Pressure transducer, Accelerometer, Digital Oscilloscope.
Computational Facility
Work Station
Software: Starccm+,
CFD++, Solidworks,
