| 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 |