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Shock waves in supersonic tunnel

  • Shock waves in supersonic tunnel

Shock Waves - X15 in 4 x 4 Foot Supersonic Tunnel.

Additional notes
The Fluids Laboratory is an integrated learning environment developed by IIHR-Hydroscience & Engineering for the College of Engineering of The University of Iowa.
Photograph published in Sixty Years of Aeronautical Research 1917-1977 By David A. Anderton (page 51) - a NASA publication. Picture taken from NASA Image eXchange.
Courtesy of Dr Marian Muste, IIHR - Hydroscience & Engineering, University of Iowa.

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