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Shock waves in supersonic tunnel

Shock waves in supersonic tunnel

Description

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

Author

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.

Copyright

Courtesy of Dr Marian Muste, IIHR - Hydroscience & Engineering, University of Iowa.

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.