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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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F. E. Kiddle (10)
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