Aerospace Testing Facilities in India

Aerospace Testing Facilities available in India

 
     
  Title of the Aerospace Test
Shock Tunnel No.2
     
  Name of the Organisation
IIT
     
  Name of theLab
Department of Aerospace Engineering - IITM
     
  Place of the Lab
Chennai
     
  Category of Aerospace Test Wind Tunnel Testing
     
  Sub-category of Aerospace Test NA
     
  Year of Establisment 1980
     
  Test Applications
Aerospace, Research & Development, and Industrial.
Steady and Unsteady pressure measurements
Flow diagnostic test
Heat transfer measurements
     
  Test Special Features
Test Section size and shape: Shock tube is rectangular 40mm x 80mm Shock tunnel is circular nozzle exit of 300mm-enclosed free jet type
Speed range / Mach number range: Speed in the shock tube typical 3500m/s
Mach number range: Mach number 5.5 in the Straight through mode; Mach number up to 13 in the Reflected mode 
Enthalpy level in the shock tunnel : Upto 6.0MJ /kg
     
  Other Test Information
Type of tunnel: Combustion driven shock tube/shock tunnel
Fully instrumented for pressure and heat transfer measurements
     
  Contact Person / Institution
The Director
Indian Institute of Technology (IIT), Madras
Sardar Patel Rd, 
Chennai, Tamil Nadu 600036
Contact No.: +91-44 -2257 8280
Fax No.: +91-44-22574002
Email: kurian@ae.iitm.ac.in
Website: http://www.iitm.ac.in/ 
     
     
     
     
 
Copyright 2012-16 AR&DB.
All rights reserved
Designed,Developed and Maintained by Dr.M.Madhusudhan
Principal Investigator & Associate Professor, Department of Library and Information Science
University of Delhi, Delhi-110007

Disclaimer