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Flow characteristics in an expansion tunnel as inferred from velocity measurementsA photoionization technique was used to study flow characteristics in an expansion tunnel. Vertical surveys of the axial component of flow velocity just downstream from the nozzle exit were obtained, and estimates of freestream density were inferred from the velocity measurement technique. The pitot pressure was measured and compared to the average axial component of velocity as a function of time for the two cases when air and CO2 were used as test gases. Vertical velocity and static density profiles at the nozzle exit are presented for the case when CO2 was used as test gas. Experimental results were used to determine the diameter and uniformity of the test core at the nozzle exit and the duration of the quasi-steady flow period. These data are relevant to evaluation of the suitability of operating an expansion tube as an expansion tunnel. The expansion tunnel is an expansion tube with a conical nozzle positioned at the exit of the acceleration section, so that nozzle entrance flow conditions are hypersonic and characterized by hypervelocity.
Document ID
19770064256
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Miller, C. G.
(NASA Langley Research Center Hampton, VA, United States)
Friesen, W. J.
(NASA Langley Research Center Space Systems Div., Hampton, Va., United States)
Date Acquired
August 9, 2013
Publication Date
September 1, 1977
Publication Information
Publication: AIAA Journal
Volume: 15
Subject Category
Aerodynamics
Accession Number
77A47108
Distribution Limits
Public
Copyright
Other

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