Aerospace Testing Facilities in India

Aerospace Testing Facilities available in India

  Title of the Aerospace Test
0.3 m Trisonic Wind Tunnel
  Name of the Organisation
  Name of theLab
National Aerospace Laboratories - NAL
  Place of the Lab
  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
  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

  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

  Contact Person / Institution
The Director
National Aerospace Laboratories,  Kodihalli 
Bangalore - 560 017 
Contact No.: +91- 080-25086001
Fax No.: +91- 080-25269611
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