Engine Research Building Wind Tunnels
(C-1998-01784): The 15 cm x 15 cm Supersonic Wind Tunnel in Room W-6 is useful for a variety of studies, including the behavior of supersonic shock waves.
Credit: NASA
Image Number: C-1998-01784
Date: August 26, 1994
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Uploaded on August 1, 2013
Taken on August 26, 1994
Engine Research Building Wind Tunnels
(C-1998-01784): The 15 cm x 15 cm Supersonic Wind Tunnel in Room W-6 is useful for a variety of studies, including the behavior of supersonic shock waves.
Credit: NASA
Image Number: C-1998-01784
Date: August 26, 1994
15,311
views
0
faves
0
comments
Uploaded on August 1, 2013
Taken on August 26, 1994