Aerospace Testing Facilities in India

Aerospace Testing Facilities available in India

 
     
  Title of the Aerospace Test
Wind Tunnel No.3
     
  Name of the Organisation
BIT
     
  Name of theLab
Department of Space Engineering and Rocketry - BITM
     
  Place of the Lab
Ranchi
     
  Category of Aerospace Test Wind Tunnel Testing
     
  Sub-category of Aerospace Test Subsonic Wind Tunnel
     
  Year of Establisment 2007
     
  Test Applications
Aerospace and Research & Development.
Total and Static Pressures
Flow Visualization
     
  Test Special Features
Test Section size and shape: 2" Conical 
Speed range / Mach number range: 1.0 - 2.0 Mach Number
Reynolds number range (per m):2.5 x 10^7 - 10^8; 2 x 10^7 -4 x 10^7
Pressure fluctuation level(if high speed, % Cprms):0.01 at M=2.0
Typical test duration : (15 - 30) sec
Stagnation pressure & Temperature range: 1 - 7 x 10^5 N/m^2, 283 - 300 K
     
  Other Test Information
 Type of Tunnel - Supersonic Free Jet, Wind, Intermittent, and Horizontal
Compressors, Air Drier, Pressure pickups, Static pressure probe, Total Probe, B & W Schlieren system, Digital Camera
     
  Contact Person / Institution
 Vice Chancellor
Birla Institute of Technology - BIT, Mesra,
Ranchi, Jharkhand- 835 215
Contact No.:+91- 651 2275444/2275896
Fax: 0651 2275401
Email:vc@bitmesra.ac.in
Website:< a href="https://www.bitmesra.ac.in/Default.aspx?this=1">https://www.bitmesra.ac.in/Default.aspx?this=1
     
     
     
     
 
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