High-speed Wind-tunnel Tests on Models of Four Single-engined Fighters (Spitfire, Spiteful, Attacker and Mustang) Parts 1-5

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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


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