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Performance and operating characteristics of the arc-driven Langley 6-inch shock tubePerformance characteristics for the arc-driven Langley 6-inch shock tube were determined for driver energies from 0.62 to 5 MJ. Voltage, current and pressure histories of the arc driver were recorded, and driver efficiencies were determined from measured shock velocities. Time-resolved spectra for test gases of air, carbon monoxide, xenon, and a mixture of 80 percent helium and 20 percent hydrogen are presented.
Document ID
19720021556
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Nealy, J. E.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1972
Subject Category
Facilities, Research, And Support
Report/Patent Number
L-8312
NASA-TN-D-6922
Report Number: L-8312
Report Number: NASA-TN-D-6922
Accession Number
72N29206
Funding Number(s)
PROJECT: RTOP 117-07-04-09
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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