| dc.contributor.author | W. A. Mair et al | en_US |
| dc.date.accessioned | 2014-10-21T15:55:33Z | |
| dc.date.available | 2014-10-21T15:55:33Z | |
| dc.date.issued | 1945 | en_US |
| dc.identifier.other | ARC/R&M-2535 | en_US |
| dc.identifier.uri | https://reports.aerade.cranfield.ac.uk/handle/1826.2/3821 | |
| dc.description.abstract | Part I - Tests on the Spitfire I. Part II - Tests on the Spiteful (F. 1/43). Part III - Tests on Cabins for the Spiteful. Part IV - Tests on the Attacker (E. 10/44). Part V - Tests on the Mustang I. This report describes measurements of lift, drag, and pitching moment made in the R.A.E. High Speed Wind Tunnel on models of the Spitfire, Spiteful (F.1/43), Attacker (E.10/44), and Mustang. On the Spiteful model, pressure distributions on the front radiator flap were also measured. An introduction (written in 1949) gives a general account of the tests described in the separate parts of the report. | en_US |
| dc.relation.ispartofseries | Aeronautical Research Council Reports & Memoranda | en_US |
| dc.title | High-speed Wind-tunnel Tests on Models of Four Single-engined Fighters (Spitfire, Spiteful, Attacker and Mustang) Parts 1-5 | en_US |