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Effect of inlet geometry on flow-angle characteristics of miniature total-pressure tubesInlet nozzle geometry effects on subsonic flow characteristics of miniature total pressure tubes including pitot tube static and dynamic pressure and flow velocity measurements
Document ID
19710021709
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Dudzinski, T. J. (NASA Lewis Research Center Cleveland, OH, United States)
Krause, L. N. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1971
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-TN-D-6406
E-6161
Report Number: NASA-TN-D-6406
Report Number: E-6161
Accession Number
71N31185
Funding Number(s)
CONTRACT_GRANT: 720-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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