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Investigation of an anomalous flow condition of the Langley pilot model expansion tubeFree-stream flow velocity measurements were made in the Langley pilot model expansion tube during the test flow interval. During this interval, an anomalous dip in pitot pressure occurs for the expansion tube operating conditions employed. Within the test flow interval, the main conclusions reached from comparison of the measured flow velocity, pitot pressure, and tube wall pressure are: the variations which occur in velocity and wall pressure are small compared with the variations in pitot pressure; a corresponding dip in the derived flow density is associated with the dip in pitot pressure; and the value of the average density over the interval, which results from the expansion from the shocked intermediate chamber condition, is approximately one-half of the value that can result from only an isentropic process.
Document ID
19740023645
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Friesen, W. J.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
August 1, 1974
Subject Category
Fluid Mechanics
Report/Patent Number
L-9633
NASA-TN-D-7704
Report Number: L-9633
Report Number: NASA-TN-D-7704
Accession Number
74N31758
Funding Number(s)
PROJECT: RTOP 502-27-01-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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