dc.contributor.author |
A. Simons |
en_US |
dc.contributor.author |
C. K. Roberts |
en_US |
dc.date.accessioned |
2014-10-21T15:53:30Z |
|
dc.date.available |
2014-10-21T15:53:30Z |
|
dc.date.issued |
1952 |
en_US |
dc.identifier.other |
ARC/R&M-2913 |
en_US |
dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/3474 |
|
dc.description.abstract |
Tests have been carried out to determine the performance of a typical Whittle compressor (produced in 1944) as used in the W2/700 series of engines. At 1,500 ft/sec tip speed the overall pressure ratio (total head) was 4.27 and the adiabatic efficiency was 75.6 per cent at a mass flow of 36.3 lb/sec. The overall efficiency fails rapidly from 79.6 per cent at 1,400 ft/sec to 75.6 per cent at 1,500 ft/sec due to choking of the outer half of the impeller eye. The maximum diffuser efficiency is approximately 80 per cent at a tip speed of 1,500 ft/sec. |
en_US |
dc.relation.ispartofseries |
Aeronautical Research Council Reports & Memoranda |
en_US |
dc.title |
Tests on a typical whittle compressor |
en_US |