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Analysis of the flow in a 1-MJ electric-arc shock tunnelIn the electric-arc-heated shock tunnel, the facility performance over a range of shock Mach numbers from 7 to 19 was evaluated. The efficiency of the arc-heated driver is deduced using an improved form of the shock tube equation. A theoretical and experimental analysis is made of the tailored-interface condition. The free stream properties in the test section, with nitrogen as the test gas, are evaluated using a method based on stagnation point, heat transfer measurements.
Document ID
19720017640
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Reller, J. O., Jr. (NASA Ames Research Center Moffett Field, CA, United States)
Reddy, N. M. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1972
Subject Category
Facilities, Research, And Support
Report/Patent Number
NASA-TN-D-6865
A-4341
Report Number: NASA-TN-D-6865
Report Number: A-4341
Accession Number
72N25290
Funding Number(s)
PROJECT: RTOP 117-07-04-15-00-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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