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Annular arc accelerator shock tubeAn annular arc accelerator shock tube employs a cold gas driver to flow a stream of gas from an expansion section through a high voltage electrode section to a test section, thus driving a shock wave in front of it. A glow discharge detects the shock wave and actuates a trigger generator which in turn fires spark-gap switches to discharge a bank of capacitors across a centered cathode and an annular anode in tandem electrode sections. The initial shock wave passes through the anode section from the cathode section thereby depositing energy into the flow gas without the necessity of any diaphragm opening in the gas flow from the expansion section through the electrode sections.
Document ID
19770003129
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Leibowitz, L. P.
(JPL)
Date Acquired
August 8, 2013
Publication Date
October 5, 1976
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
Patent Application Number: US-PATENT-APPL-SN-521620
Patent Number: NASA-CASE-NPO-13528-1
Patent Number: US-PATENT-3,983,749
Accession Number
77N10071
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-NPO-13528-1|US-PATENT-3,983,749
Patent Application
US-PATENT-APPL-SN-521620
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