The HSWT is a tri-sonic, blow down tunnel with a Mach number range of 0.3 to 4.8. The test section measures 4’ X 4’ X 6’ for transonic testing and 4’ X 4’ X 5’ for supersonic testing.
Lockheed Martin High Speed Wind Tunnel
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By Mike1989 @ 2012-06-21 11:08:43