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As a NASA aerospace engineer I conducted numerous tests in the 8x6 Foot Supersonic Tunnel from 1966 through the 80's. The Mach number range for this particular wind tunnel was 0.36 to 2.0.
I also conducted tests in the 10x10 Supersonic Wind Tunnel. The Mach number range for that tunnel was 2.0 to 3.5.
fastdancer77 2 years ago
@fastdancer77
The 4th WOW to you.
grenadehehe 2 years ago
My Dad works there.
lampstink5 4 years ago
I just went there today!
havannah45 4 years ago
Me2! my dad works in the BIG building
cowsrock99 4 years ago
he works there!?
AWESOME!!!!!!!!!!!!
havannah45 4 years ago
yHAW!
cowsrock99 4 years ago
:D:D:D:D!!!
havannah45 4 years ago