dc.contributor.author |
A. R. G. Mundell |
en_US |
dc.date.accessioned |
2014-10-21T15:50:57Z |
|
dc.date.available |
2014-10-21T15:50:57Z |
|
dc.date.issued |
1973 |
en_US |
dc.identifier.other |
ARC/R&M-3755 |
en_US |
dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/3034 |
|
dc.description.abstract |
The geometry is given of a probe capable of measuring stagnation pressure directly in a supersonic flow, by means of an isentropic compression. Tests have shown that such a probe can indicate the local stagnation pressure to within 0.1 per cent for Mach numbers up to 2.2. Above M = 2.2 the pressure recovery begins to fall from unity and precalibration becomes necessary. |
en_US |
dc.relation.ispartofseries |
Aeronautical Research Council Reports & Memoranda |
en_US |
dc.title |
Tests on probes designed to measure stagnation pressure directly in a supersonic stream |
en_US |