Aerospace Testing Facilities available in India
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| Title of the Aerospace Test |
0.5m Base Flow 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 | Twin jet interaction A/c after body flow studies |
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| Test Special Features | Test section: 524 mm dia Nozzle: Variable geometry Operation: Intermittent Blow down type Free stream Mach number range: 0.5 to 4.0 Jet nozzle flow : up to 150psi |
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| Other Test Information | Measurement capability: Reynolds number range: 10-50 million/m Model support Nozzle inner body, 127 mm dia Test duration:30-40sec Conventional Digital manometer, 32 port ESP scanner, 35 channel simultaneous unsteady pressure DAQ Flow Diagnostics:Particle Image Velocimetry (PIV), Schlieren, 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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