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Showing 10 out of a total of 460 results for collection: Aeronautical Research Council Reports & Memoranda.
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The performance after power failure of a helicopter with blade pitch control Parts I and II
F. O'Hara
;
H. A. Mather
(
1951
)
An axially symmetric analogue for general three-dimensional boundary layers
J. C. Cooke
(
1959
)
The spinning of model aircraft and the prediction of full-scale spin and recovery characteristics
G. E. Pringle
;
D. J. Harper
(
1952
)
Theoretical load distributions on fin-body-tailplane arrangements in a side-wind
J. Weber
;
A. C. Hawk
(
1954
)
Tests concerning novel designs of blades for axial compressors Part 1 blades designed for increased work at root and tip Part 2 blades designed to operate in a parabolic axial velocity distribution
S. J. Andrews
;
R. A. Jeffs
;
E. L. Hartley
(
1951
)
The effect of a spike protruding in front of a bluff body at supersonic speeds
D. Beastall
;
J. Turner
(
1952
)
Wind-tunnel tests on the NACA 63A009 aerofoil with distributed suction over the nose
N. Gregory
;
W. S. Walker
(
1952
)
The interaction between shock waves and boundary layers at the trailing edge of a double-wedge aerofoil at supersonic speed
B. D. Henshall
;
R. F. Cash
(
1955
)
The design and testing of an axial-flow compressor having different blade profiles in each stage
A. D. S. Carter
;
R. C. Turner
;
D. W. Sparkes
;
R. A. Burrows
(
1957
)
Experiments at M = 1.41 on elliptic cones with supersonic leading edges
E. W. E. Rogers
;
C. J. Berry
(
1955
)
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J. Weber (13)
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H. C. Garner (8)
N. Gregory (8)
W. G. Molyneux (8)
W. S. Walker (8)
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