NASA NTRS · 19720000542
A stagnation pressure probe for use in supersonic flow
Abstract
Probe 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.
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Goodyer, M. J.. 1972-09-01. A stagnation pressure probe for use in supersonic flow. https://ntrs.nasa.gov/citations/19720000542
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