Aerospace Testing Facilities in India

Aerospace Testing Facilities available in India

  Title of the Aerospace Test
Wind Tunnel No.3
  Name of the Organisation
  Name of theLab
Department of Space Engineering and Rocketry - BITM
  Place of the Lab
  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
Website:< a href="">
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