Aerospace Testing Facilities available in India
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| Title of the Aerospace Test |
Subsonic Wind Tunnel No.1 |
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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 | 1965 | |
| Test Applications | Aerospace and Non-aerospace Research & Development Laboratory classes for students Static Pressures Type of tests performed: Tuft flow visualization Smoke flow visualization Laser sheet flow visualization Static Pressure measurement |
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| Test Special Features | Test section size : 150mm x 300mm Speed range / Mach number range: 1 m/s - 10 m/s Reynolds number range (per m): 7 x 10 power of 5 to 7 x 10 power of 6 Freestream turbulence level(If Low speed tunnel): 0.5 % |
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| Other Test Information | Ranges of Pitch, Roll and Yaw : + 300 Pitch Typical test duration : Continuous Type of Tunnel - Low Speed, Wind, Continuous, and Horizontal Instrumentation: Multi-tube Manometer, Pressure transducers, Smoke generator, 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:https://www.bitmesra.ac.in/Default.aspx?this=1 |
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