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A stagnation pressure probe for use in supersonic flowProbe was developed which is capable of recording true stagnation pressure in supersonic and subsonic flows. Static pressure orifices in the compression surface allow probe to be used as combined flow direction and stagnation pressure sensor.
Document ID
19720000542
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Goodyer, M. J.
Date Acquired
August 6, 2013
Publication Date
September 1, 1972
Subject Category
Mechanics
Report/Patent Number
LAR-11139
Report Number: LAR-11139
Accession Number
72B10543
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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