Aerospace Testing Facilities available in India
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| Title of the Aerospace Test |
Subsonic Wind Tunnel No.2 |
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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 | 1975 | |
| Test Applications | Aerospace and Non-aerospace R & D Laboratory classes for students Project for ME students PhD students Sponsored projects Type of tests performed: Tuft flow visualization Oil flow visualization Static Pressure measurement Unsteady Pressure measurement Force and Moment measurement |
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| Test Special Features | Test Section size : 600 mm X 600 mm Speed range : 5 m/s – 30 m/s Reynolds number range (per m): 3 x 105 to 2 x 106 Freestream turbulence level : 0.5 % Angle of attack : 0 to 60 degrees Test control parameters: Multi-tube Manometer, Pressure Transducers, Pressure scanners Unsteady pressure Transducers (Kulite Make) 6 component Strain gauge balance, Digital Camera Electronic speed controller Signal conditioners NI Cards |
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| Other Test Information | Data Acquisition Systems: PC Based Data Acquisition Systems With low and high speed NI DAQ, Labview Special test rigs and test techniques developed: PC controlled incidence mechanism Upgradation: Automation through DAS |
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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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