Project Description

Aerodynamics Laboratory

The heart of Aerospace Engineering, the Aerodynamics Laboratory provides students with hands-on experience and practical learning on various aerodynamic concepts. The main areas of study are force and moment measurement techniques and different flow visualization techniques. In addition, the lab has the facility to conduct experiments on jet flows, flow separation and boundary layer studies. The laboratory provides the students with a venue to pursue their interests through experiments and projects

The laboratory features a subsonic wind tunnel and a water tunnel with a maximum flow velocity of 50 m/s. The lab is also equipped with various apparatus for flow measurements, such as multi tube manometers, pitot-static tubes, pitot rake, multi-stage traverse, etc.

Faculty In-charge:

Dr. Atal Bihari Harichandan

Technical Asst. In-charge:

Mr. B.N. Das

  • Subsonic Wind Tunnel (Test Section Size :600mmx600mmx2000mm)
  • Water Flow Channel Apparatus