Aerospace Testing Facilities available in India
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| Title of the Aerospace Test |
5" X 7" supersonic wind tunnel |
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| Name of the Organisation |
IISc |
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| Name of theLab |
Department of Aerospace Engineering |
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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 | Supersonic wind tunnel | |
| Year of Establisment | NA | |
| Test Applications | Aerospace |
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| Test Special Features | Test Section size and shape: 5" X 7" Mach number range: 2D convergent –divergent nozzle of M=1.2 to 4 Reynolds number range (per m): 1.3x10^10 Test Control Parameters: Test duration 60S Constant stagnation pressure (ambient) Constant stagnation Temperature (ambient) Vacuum tank volume of 300m3 at 1 Torr Pressure measurement capabilities with ESP scanner, Kulite, individual chip based transducer like Honeywell, Measurement Computing etc. 350mm dia vacuum isolation knife edge gate va |
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| Other Test Information | Type of Tunnel:Intermittentindraft type. Instrumentation: Color Schlierenvideo recording system Data Acquisition System: 1616 FS Measurement computing USB based data acquisition system. Dasylab software for data capture. |
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| Contact Person / Institution | The Director Indian Institute of Science (IISc) Bangalore - 560012 Contact No.: +91-80 -23600690 Fax: + 91 - 80 - 23600936 E-mail: diroff@admin.iisc.ernet.in Website:http://www.iisc.ernet.in/ |
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