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Showing 7 out of a total of 37 results for community: Aeronautical Research Council. (0.109 seconds)

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The Effect of Tab Mass-balance on Flutter Part I Ternary Tailplane-Elevator-Tab Flutter Part II Experiments on the Influence of Tab Mass-balance on Flutter

G. H. L. Buxton; G. D. Sharpe; C. Scruton; P. M. Ray; D. V. Dunsdon (1946)
Flight tests on Hurricane II, Z.3687 fitted with special wings of 'low-drag' design

R. H. Plascott; D. J. Higton; F. Smith; A. R. Bramwell (1946)
Measurements of the degree of smoothness attained in a laminar-flow wing speciment (Short Bros.)

R. B. Coles (1946)
Investigation of the flow past finite wedges of 20 deg. and 40 deg. apex angle at subsonic and supersonic speeds, using a Mach-Zehnder interferometer with appendix: sensitivity and accuracy of the interference method applied to pressure measurements

D. C. Pack; E. Groth (1946)
Further wind tunnel tests on a 30 per cent. symmetrical suction aerofoil with a movable flap

N. Gregory; W. S. Walker (1946)
24-ft. tunnel tests on a Rotol wooden Spitfire propeller. Test results, and data for single radius calculations

A. B. Haines; P. B. Chater (1946)
Influence of Tuned Dampers on Flexure-Aileron Flutter. Parts I-III.

R.A. Frazer et al (1946)

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- 1946 (37)