dc.contributor.author |
M. J. Goodyer |
en_US |
dc.date.accessioned |
2014-10-21T15:50:59Z |
|
dc.date.available |
2014-10-21T15:50:59Z |
|
dc.date.issued |
1973 |
en_US |
dc.identifier.other |
ARC/R&M-3762 |
en_US |
dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/3041 |
|
dc.description.abstract |
The probe decelerates a portion of the supersonic free stream into the subsonic range within a distributed compression fan. Stagnation pressure is sampled in the region of subsonic flow using a pitot tube. Pressure recovery has been measured over the Mach number range 1.5 to 2.5, a typical value being 0.999 at a Mach number of 1.88. The probe is usefully insensitive to misalignment with the free stream and pressure tappings in the compression surface allow it to be used also as a flow-direction sensor. |
en_US |
dc.relation.ispartofseries |
Aeronautical Research Council Reports & Memoranda |
en_US |
dc.title |
A new probe for the direct measurement of stagnation pressure in supersonic flow |
en_US |