Aerospace Testing Facilities available in India
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Title of the Aerospace Test |
0.5m Hypersonic 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 | Hypersonic Wind Tunnels | |
Year of Establisment | NA | |
Test Applications | Aerospace & Industrial |
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Test Special Features | Mach number range: Contoured axi-symmetric nozzle of Mach 8.0 Reynolds number range (per m): 3.45x104 to 1.05X107 (based on jet dia) Test Control Parameters: Servo, electro-hydraulic model incidence and injection system with <1s response time Model Incidence Range : -6° to +24° (accuracy of 0.1°) Test Duration 10 seconds Air cooled reciprocating compressor with acoustic canopy (Burckhardt Compression) : Capacity 411Nm3/hr High pressure air driers with dew point of 180K. Maximum stag |
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Other Test Information | Type of Tunnel: Pressure - vacuum, Intermittent blow type Instrumentation: Color Schlieren flow visualization system with 300mm light beam Data Acquisition System: 16 bit Data acquisition at 1M Sample /sec (USB based Personal DAQ book 3000series, HBM, Vishay and Scad 500) |
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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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