Aerospace Testing Facilities available in India
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| Title of the Aerospace Test |
Wind Tunnel No.3 |
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| Name of the Organisation |
BIT |
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| Name of theLab |
Department of Space Engineering and Rocketry - BITM |
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| Place of the Lab |
Ranchi |
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| Category of Aerospace Test | Wind Tunnel Testing | |
| Sub-category of Aerospace Test | Subsonic Wind Tunnel | |
| Year of Establisment | 2007 | |
| Test Applications | Aerospace and Research & Development. Total and Static Pressures Flow Visualization |
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| Test Special Features | Test Section size and shape: 2" Conical Speed range / Mach number range: 1.0 - 2.0 Mach Number Reynolds number range (per m):2.5 x 10^7 - 10^8; 2 x 10^7 -4 x 10^7 Pressure fluctuation level(if high speed, % Cprms):0.01 at M=2.0 Typical test duration : (15 - 30) sec Stagnation pressure & Temperature range: 1 - 7 x 10^5 N/m^2, 283 - 300 K |
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| Other Test Information | Type of Tunnel - Supersonic Free Jet, Wind, Intermittent, and Horizontal Compressors, Air Drier, Pressure pickups, Static pressure probe, Total Probe, B & W Schlieren system, Digital Camera |
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| Contact Person / Institution | Vice Chancellor Birla Institute of Technology - BIT, Mesra, Ranchi, Jharkhand- 835 215 Contact No.:+91- 651 2275444/2275896 Fax: 0651 2275401 Email:vc@bitmesra.ac.in Website:< a href="https://www.bitmesra.ac.in/Default.aspx?this=1">https://www.bitmesra.ac.in/Default.aspx?this=1 |
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