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Description and initial operating performance of the Langley 6-inch expansion tube using heated helium driver gasA general description of the Langley 6-inch expansion tube is presented along with discussion of the basic components, internal resistance heater, arc-discharge assemblies, instrumentation, and operating procedure. Preliminary results using unheated and resistance-heated helium as the driver gas are presented. The driver-gas pressure ranged from approximately 17 to 59 MPa and its temperature ranged from 300 to 510 K. Interface velocities of approximately 3.8 to 6.7 km/sec were generated between the test gas and the acceleration gas using air as the test gas and helium as the acceleration gas. Test flow quality and comparison of measured and predicted expansion-tube flow quantities are discussed.
Document ID
19750022129
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Moore, J. A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1975
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NASA-TM-X-3240
L-9900
Report Number: NASA-TM-X-3240
Report Number: L-9900
Accession Number
75N30202
Funding Number(s)
PROJECT: RTOP 502-27-01-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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