Aerospace Testing Facilities in India

Aerospace Testing Facilities available in India

  Title of the Aerospace Test
Aerodynamic Testing
  Name of the Organisation
  Name of theLab
Gas Turbine Research Establishment - GTRE
  Place of the Lab
  Category of Aerospace Test Aerodynamic
  Sub-category of Aerospace Test Axial Flow Compressor
  Year of Establisment 1980
  Test Applications
Characterisation of Axial Flow Compressor
  Test Special Features
6MW Gas Turbine Driven Test facility
Speed: 15000rpm (max)
Mass Flow: 35 to 40 kg/s

Data Acquisition like Pressure, Temperature
Health monitoring parameters like Vibration, Tip Clearance, Dynamic Pressure and Strain Gauging.

  Other Test Information
Test facility being used for 
Design validation of Axial Flow Compressors developed by GTRE
Surge Margain Estimation
Both Clean and Distortion tests are possible.
  Contact Person / Institution
The Director
Gas Turbine Research Establishment (GTRE)
Defence Research and Development Organization (DRDO)
Ministry of Defence
PO Box 9302, CV Raman Nagar 
Bangalore-560 093
E-mail :
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