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Showing 10 out of a total of 924 results for community: Aeronautical Research Council.
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Low-speed-tunnel model tests on the flow structure behind a delta-wing aircraft and a 40 deg swept-wing aircraft at high incidences
D. A. Kirby
;
A. Spence
(
1955
)
A direct iteration method for the calculation of the velocity distribution of bodies of revolution and symmetrical profiles
F. Vandrey
(
1951
)
Aerodynamic Forces on Biconvex Aerofoils Oscillating in a Supersonic Airstream + Effect of Thickness on the Aerodynamic Forces on Biconvex Aerofoils Oscillating in a Supersonic Airstream, and Calculation of Forces for Aerofoil with Flap
W. P. Jones
;
Sylvia W. Skan
(
1951
)
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
)
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B. D. Henshall (13)
D. W. Holder (13)
H. C. Garner (13)
J. Weber (13)
W. G. Molyneux (12)
Aeronautical Research Council (11)
E. H. Mansfield (11)
S. Neumark (11)
G. E. Gadd (10)
L. C. Woods (10)
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