Published February 1, 1973
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Cryogenic shock tube
Abstract
Two shock tubes have been developed which allow for partial or full immersion of the test sections within a cryogenic bath. One tube is used for the study of shock-wave interactions with strong density gradients, and the other to obtain very large shock Mach numbers with ideal gas conditions in all flow regions.
Additional Information
©1973 American Institute of Physics. This research effort has been sponsored by the Air Force Office of Scientific Research, Grant No. AF-AFOSR-71-2092.Files
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