Aerospace Testing Facilities available in India
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| Title of the Aerospace Test |
0.3 m Trisonic Wind Tunnel |
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| Name of the Organisation |
CSIR |
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| Name of theLab |
National Aerospace Laboratories - NAL |
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| Place of the Lab |
Bangalore |
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| Category of Aerospace Test | Wind Tunnel Testing | |
| Sub-category of Aerospace Test | NA | |
| Year of Establisment | 1996 | |
| Test Applications | Intake studies – buzz control Shock boundary layer interaction studies PSP Studies Density field studies |
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| Test Special Features | Test section size: 0.3 x 0.3 m Supersonic 0.381 x 0.3 m - Transonic Mach number range:0.2 – 4.0. Operation Intermittent blow down type Reynolds number range 8 x 106 to 60 x 106 / meter Model support Sting, Wall mounted |
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| Other Test Information | Measurement capability: Conventional Digital manometer, 32 port ESP scanner, 35 channel simultaneous unsteady pressure DAQ Flow Visualization: Surface oil flow, Dynamic Schlieren Flow Diagnostic: Pressure Sensitive paint (PSP), Background Oriented Schlieren (BOS) Experimental Aerodynamics Division - EAD |
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| Contact Person / Institution | The Director National Aerospace Laboratories PB.no.1779, Kodihalli Bangalore - 560 017 Contact No.: +91- 080-25086001 Fax No.: +91- 080-25269611 Email: director@nal.res.in Website: http://www.nal.res.in |
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