Aerospace Testing Facilities available in India
 |
||
| Title of the Aerospace Test |
0.3m Hypersonic Wind Tunnel |
|
| Name of the Organisation |
IISc |
|
| Name of theLab |
Department of Aerospace Engineering |
|
| Place of the Lab |
Bangalore |
|
| Category of Aerospace Test | Wind Tunnel Testing | |
| Sub-category of Aerospace Test | Hypersonic Wind Tunnels | |
| Year of Establisment | NA | |
| Test Applications | Aerospace & Industrial |
|
| Test Special Features | Test Section size and shape: Enclosed free-jet size of 0.3m dia. Mach number range: Contoured axi-symmetric nozzle of Mach 5.4,6.5,7.0,8.35,and 10.2 Reynolds number range (per m): 3.45x10^4 to 1.05X10^7 (based on jet dia) Test Control Parameters: Servo, electro-hydraulic model incidence and injection system with <1s response time Model Incidence Range : -10° to +20° (accuracy of 0.1°) Test Duration 30 seconds Water cooled, reciprocating compressor(Norkwalk, USA) : capacity 424Nm |
|
| Other Test Information | Type of Tunnel: Pressure - vacuum, Intermittent blow type Instrumentation: Color Schlieren flow visualization system Data Acquisition System: 16 bit Data acquisition at 1M Sample /sec (PCI based DAQ board 2000 series) |
|
| 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/ |
|