NASA NTRS · 19740024765
Stagnation pressure probe
Abstract
A method and apparatus for measuring the stagnation pressure of supersonic velocity gas streams without the generation of shock waves which interfere with such measurements are given. The technique is insensitive to the type of gas and Mach number and is therefore particularly useful in the study of jet engine exhausts.
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Goodyer, M. J.. 1974-09-03. Stagnation pressure probe. https://ntrs.nasa.gov/citations/19740024765
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