Aerospace Testing Facilities available in India
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| Title of the Aerospace Test |
Medium Size Wind Tunnel |
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| Name of the Organisation |
MIT |
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| Name of theLab |
Madras Institute of Technology - MIT, Anna University |
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| Place of the Lab |
Chennai |
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| Category of Aerospace Test | Wind Tunnel Testing | |
| Sub-category of Aerospace Test | NA | |
| Year of Establisment | 1985 | |
| Test Applications | Aerospace, Non-aerospace, Research & Development and Industrial. Boundary layer flow studies |
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| Test Special Features | Test Section size and shape: 0.6 x 0.6 x 2/4/6 m Rectangular Cross-section Speed range : Up to 30 m/sec Reynolds number range (per m): Up to 4.125 million per meter Free-stream turbulence level (if low speed): Good |
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| Other Test Information | Test section modified to facilitate Boundary layer studies. Multi-channel pressure scanner Manometers Strain measurements (Spidpak 3013 E - Pro package) Miniature Quatz Pressure Transducer Wind tunnel balance Digital storage Oscilloscope |
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| Contact Person / Institution | Dean Madras Institute of Technology Anna University, Chrompet, Chennai - 600 044 Contact No.:+91-44-22237038 Fax No.: +91-44-22237038 Email: sridhar@mitindia.edu Website:http://mitindia.edu/home.html |
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