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Showing 10 out of a total of 105 results for community: Aeronautical Research Council.
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An approximate method of calculating the laminar boundary layer in two-dimensional incompressible flow
M. R. Head
(
1957
)
Measurements of the direct hinge-moment derivatives at subsonic and transonic speeds for a cropped delta wing with oscillating flap
J. B. Bratt
;
C. J. W. Miles
;
R. F. Johnson
(
1957
)
The formation of regions of separated flow on wing surfaces Part 1 low-speed tests on a two-dimensional unswept wing with a 10 per cent thick RAE 101 section Part 2 laminar-separation bubbles and the mechanism of the leading-edge stall
L. F. Crabtree
(
1957
)
The effect of reynolds number on the performance of a single-stage compressor
A. D. S. Carter
;
C. E. Moss
;
G. R. Green
;
G. G. Annear
(
1957
)
An experimental investigation of leading-edge flow separation from a 4 per cent thick two-dimensional biconvex aerofoil
B. D. Henshall
;
R. F. Cash
(
1957
)
Low-speed experiments on the wake characteristics of flat plates normal to an air stream
R. Fail
;
J. A. Lawford
;
R. C. W. Eyre
(
1957
)
A theory of the separated flow from the curved leading edge of a slender wing
J. H. B. Smith
(
1957
)
Body freedom flutter of ground-launched rocket models at supersonic and high subsonic speeds
D. R. Gaukroger
(
1957
)
Wind-tunnel tests on the use of distributed suction for maintaining laminar flow on a body of revolution
N. Gregory
;
W. S. Walker
(
1957
)
Flutter of an all-moving tailplane
E. G. Broadbent
;
Margaret Williams
(
1957
)
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J. H. Horlock (4)
K. G. Winter (4)
R. F. Cash (4)
B. D. Henshall (3)
P. F. Ashwood (3)
R. Parker (3)
W. G. Molyneux (3)
A. D. S. Carter (2)
A. J. Alexander (2)
A. Stanbrook (2)
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Date Issued
1957 (105)