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Some notes on the flow patterns observed over various swept-back wings at low Mach numbers (in the R.A.E. 10-ft x 7-ft high speed tunnel)

A. B. Haines (1954)
Tests in the Royal Aircraft Establishment 10-ft x 7-ft high-speed tunnel on 50-deg swept-back wings. Part I. Three of 7.5 per cent thickness. Part II. One of 7.5 per cent thickness with stall fences and leading-edge chord extension

A. B. Haines; C. W. Rhodes (1954)

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- A. B. Haines (2)
- C. W. Rhodes (1)
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- 1954 (2)