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High-speed Wind-tunnel Tests on Modelsnof Four Single-engined Fighters (Spitfire, Spiteful, Attacker and Mustang) Parts Ⅰ— 5

机译:四个单引擎战斗机(喷火,恶意,攻击者和野马)部件的高速风洞试验Ⅰ-5

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摘要

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.l/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.

著录项

  • 作者

    W. A. MAIR;

  • 作者单位
  • 年度 1951
  • 页码 1-81
  • 总页数 81
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 工业技术;
  • 关键词

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