Aerospace Testing Facilities available in India
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| Title of the Aerospace Test |
Low Speed Wind Tunnel |
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| Name of the Organisation |
Others |
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| Name of theLab |
Jaypee Wind Engineering Application Centre - JWEAC |
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| Place of the Lab |
Guna |
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| Category of Aerospace Test | Wind Tunnel Testing | |
| Sub-category of Aerospace Test | Subsonic Wind Tunnel | |
| Year of Establisment | 2013 | |
| Test Applications | Non- aerospace and primarily for Civil Engineering applications Industrial and Research & Development. |
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| Test Special Features | Test Section size and shape: 3.5 m X 3.0 m X 22.0 m – Rectangular Speed range: 0.5 m/s to 40 m/s Reynolds number range (per m): 3.3 x 104 to 2.67 x106 Expected free stream turbulence: Typically around 10% at a height of about 90 cm under simulated open terrain condition. Terrain Simulation: Simulation of atmospheric boundary layer including profile of mean velocity, turbulence intensity and spectrum of horizontal wind speed. Special features of the tunnel: Twin- turn table facility |
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| Other Test Information | Type of tunnel: Closed circuit, low speed, boundary layer wind tunnel Instrumentation: Hot-wire anemometry system: (normal and XY – wire probe) Multi-channel high scan dynamic pressure system (512 channels; 2 Initiums; Scanners with DTC) Standered Pitot tube Six -component base balance Strain gauges and accelerometers Special instruments for control of turn-table position; traverse system and fan speed. Data acquisition system/software: Labview, Matlab; PSI pressure measurement systems; In house development GUI software |
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| Contact Person / Institution | The Director Jaypee University of Engineering & Technology A-B Road, Raghogarh, Distt. - Guna (M.P.) - 473226 Contact No.: +91- 07544-267051, 267310-314 Fax No.: +91- 07544-267011 Email: contact@uet.ac.in Website: http://www.juet.ac.in/ |
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