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Free-stream temperature, density, and pressure measurements in an expansion tube flowAn experimental study was conducted to determine test-flow conditions in the Langley pilot model expansion tube. Measurements of temperature, density, wall pressure, pitot pressure, and shock and interface velocities were compared with theoretical calculations based on various models of the flow cycle. The vibrational temperature and integrated density of the molecular oxygen component of the flow were measured by use of vacuum ultraviolet absorption techniques. These measurements indicate both the presence and possible degree of nonequilibrium in the flow. Data are compared with several simplified models of the flow cycle, and data trends are discussed.
Document ID
19730022517
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Haggard, K. V.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1973
Subject Category
Fluid Mechanics
Report/Patent Number
L-8788
NASA-TN-D-7273
Report Number: L-8788
Report Number: NASA-TN-D-7273
Accession Number
73N31249
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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