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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.

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.
Autor
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.




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This web site was launched by Prof. Michele Mossa of the Polytechnic University of Bari (Italy) with the initial support of Fondazione Caripuglia, Bari, Italy for the Research Project LIC-MON of 2003 and of the Project IMCA (Integrated Monitoring of Coastal Areas) financed by MIUR PON D.M. 593/00. Later, the initiative was supported with other Prof. Michele Mossa’s funds, most recently provided by the RITMARE Project.


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