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Analysis of flow dynamics through small diameter gas sampling systemsThe removal of gas material through a capillary opening in a surface is analyzed. The gas, from which the sample is removed, is moving past the surface at supersonic velocities. A variety of possible conditions of temperature, pressure and composition are discussed in an effort to emulate conditions that might be found at the surface of a vehicle traversing the altitude range 100-50 km, or might exist at the surface of a model in the stream of a high enthalpy wind tunnel. Aspects discussed include: (1) the throughput of the capillary for conditions of different lengths and different L/a (length/radius) ratios; (2) the total throughput when the surface in question contains many hundreds of these capillaries; (3) the effect of the capillaries upon the composition of the analyzed gas; (4) the effect of the capillary or capillaries upon the gas stream itself; and (5) the implications of the calculations upon the possible implementation of this type of device as an inlet for a mass spectrometer to be developed for analyzing the upper atmosphere.
Document ID
19840013208
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Brown, K. G.
(Old Dominion Univ. Norfolk, VA, United States)
Date Acquired
September 4, 2013
Publication Date
February 1, 1984
Subject Category
Acoustics
Report/Patent Number
NASA-CR-175447
NAS 1.26:175447
Report Number: NASA-CR-175447
Report Number: NAS 1.26:175447
Accession Number
84N21276
Funding Number(s)
CONTRACT_GRANT: NAS1-17099
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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