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High-speed wind-tunnel tests on six wings of 40-deg sweepback, with various section shapes

L. N. Holmes; A. B. Haines (1952)
Tests in the R.A.E. 10-ft x 7-ft high speed wind tunnel on drop tanks fitted to two swept-back wings Part 1 Comparison of under-wing and wing-tip installations Part 2 Comparison of various under-wing drop-tank arrangements

D. E. Hartley; A. B. Haines (1952)

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- A. B. Haines (2)
- D. E. Hartley (1)
- L. N. Holmes (1)
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- 1952 (2)