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Showing 10 out of a total of 462 results for community: Aeronautical Research Council. (0.134 seconds)

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Some examples of the application of methods for the prediction of boundary-layer transition on sheared wings

D. A. Treadgold; J. A. Beasley (1973)
An application of fast frequency-sweep excitation to the measurement of sub-critical response of a low speed wind tunnel model

C. W. Skingle; D. R. Gaukroger (1976)
An investigation of the pressure distributions on a 45 degree swept half wing including the effects of upper surface spoilers

M. D. Dobson (1971)
A laboratory comparison of three methods of personal conditioning

J.R. Allan et al (1972)
The longitudinal stability characteristics of an ogee wing of slenderness ratio = 0.35

A. G. Hepworth (1972)
Some results of wind-tunnel tests on an aerofoil section (NPL 9510) combining a 'peaky' upper surface-pressure distribution with rear loading

D.J. Hall; V.G. Quincey; R.C. Lock (1974)
A strain modified 'steady-state' creep relationship for high strength aluminium alloy

J. N. Webb (1977)
An assessment of the accuracy of subsonic linearized theory for the design of warped slender wings

Patricia J. Davies (1975)
A mean camberline singularity method for two-dimensional steady and oscillatory aerofoils and control surfaces in inviscid incompressible flow

B.C. Basu (1978)
The prediction of boundary-layer behaviour and profile drag for infinite yawed wings part 2 flow near a turbulent attachment line

B. G. J. Thompson (1974)

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