The lab provides facilities in the areas of High Speed Jet Mixing and Acoustics, Supersonic Combustion and so on. In addition to catering to the needs of undergraduate and post-graduate laboratory course needs, it caters to the research requirements of a large number of Doctoral (PhD) and Master (MTech) students. Currently 7 doctoral students are doing their research in the lab. The lab is equipped with an indigenously built Jet Acoustic Chamber, which is unique in India.
The lab also houses an intermittent, blowdown type supersonic wind tunnel. The tunnel is equipped with a dedicated computer system for tunnel control and data acquisition. This facility has already made substantial contribution in establishing new testing techniques and basic research in the area of transonic/supersonic flows.
Gas Dynamics - experimental and theoretical investigation Rarefied flowsApplied Gas Dynamics and High speed jets
Sudden expansion problems
Active and passive control of jets and base flows
Supersonic, Transonic and subsonic Aerodynamics
Supersonic blow-down wind tunnel (225mm x 175mm)
High Speed Jet Test Facility
Indigenously built Jet Acoustic Chamber.
Compressor for air supply, it can compress the air to a maximum of about 300 psi.
The lab has also acquired a high-pressure compressor which can deliver compressed air at 2000 psi.
Prof. E. Rathakrishnan- Gas Dynamics
Dr. A. Kushari - Experimental Fluid Mechanics, High speed Flows, Noise Control
Prof. E. Rathakrishnan
High Speed Aerodynamics Laboratory
Department of Aerospace Engineering
Indian Institute of Technology
Kanpur - 208 016 (UP)
Off: +91 (512) 259-7847
Lab: +91 (512) 259-7847
Fax: +91 (512) 259-7561