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21-Inch Hypersonic Wind Tunnel

Shadowgraphs such as this one of a blunt cone-flare in free flight at Mach 5 clearly revealed shock waves. The nose shock’s formation some distance ahead of a blunt body greatly reduced the heat transferred to the body at speeds above Mach 5.

 

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Credit: NASA/JPL

Image Number: 373-6678

Date:

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Uploaded on August 1, 2013
Taken on December 18, 2011