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Showing 10 out of a total of 96 results for community: Aeronautical Research Council.
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On some aspects of the use of shock tubes in aerodynamic research
B. D. Henshall
(
1955
)
Some observations of the flow over a delta-winged model with 55-deg leading-edge sweep, at Mach numbers between 0.4 and 1.8
E. P. Sutton
(
1955
)
On the stressing of multi-rib thin wings of low aspect ratio and rectangular plan-form
L. S. D. Morley
(
1955
)
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
)
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
)
Experiments at M = 1.41 on elliptic cones with supersonic leading edges
E. W. E. Rogers
;
C. J. Berry
(
1955
)
Effect of Yaw on the compressible laminar boundary layer
J. Tinkler
(
1955
)
Measurements of two-dimensional derivatives on a wing-aileron-tab system with a 1541 section aerofoil. Part 2 direct tab and cross aileron-tab derivatives
K. C. Wight
(
1955
)
A new standard for the prediction of full-scale spin and recovery characteristics from model tests
T. H. Kerr
(
1955
)
Supersonic flow past quasi-cylindrical bodies of almost circular cross-section
D. G. Randall
(
1955
)
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W. G. Molyneux (4)
D. M. Ridland (3)
F. Ruddlesden (3)
H. Hall (3)
J. K. Friswell (3)
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Aeronautical Research Council (2)
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Date Issued
1955 (96)