AERODYNAMICS LABORATORY
- Subsonic Wind tunnel
- supersonic wind tunnel
- Schlieren System
- U-Tube Manometer
- Multiple Manometer stands
- Wings of various aerofoil sections (Symmetrical & cambered aerofoils)
- Pressure Transducers with digital display
- Hele-Shaw apparatus
- Smoke Tunnel
- Water flow channel
- Angle of incidence changing mechanism
- Multi tube Manometer
- Pitot-Static Tubes
- Cylinder models (Rough and Smooth)
- Wind Tunnel balances (3 or 6 components)
- Smoke Generator
- Water flow channel
PROPULSION LABORATORY
- Jet engine
- Piston engine
- Multitube manometer
- Wind tunnel (subsonic and supersonic)
- DSA pressure scanner
- Ramjet facility
- Conical flame holder model
- Hemispherical flame holder model
- Water flow channel
- Compressor blade set
- Schlieren or Shadowgraph set up
- Convergent nozzle
- Convergent divergent nozzle
- Thruster with load cells
- High Resolution CCD Camera for Flow Visualization
- Shadowgraph Technique
AIRCRAFT SYSTEMS LABORATORY
- Serviceable Aircraft
- Hydraulic Jacks (Screw Jack)
Avionics Laboratory
- Microprocessor 8085 Kit
- Analog to Digital Converter
- MIL-Std – 1553 Data Bus
AERO ENGINE AND AIRFRAME LABORATORY
- Aircraft Piston engines
- NDT equipment