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Showing 10 out of a total of 460 results for collection: Aeronautical Research Council Reports & Memoranda.
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Part I The Effect on Transition of Isolated Surface Excrescences in the Boundary Layer. Part II Brief Flight Tests on a Vampire I Aircraft to Determine the Effect of Isolated Surface Pimples on Transition
N. Gregory
;
W. S. Walker
;
D. Johnson
(
1951
)
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
)
The subsonic flow past swept wings at zero lift without and with body
D. K�uchemann
;
J. Weber
(
1953
)
On the stressing of multi-rib thin wings of low aspect ratio and rectangular plan-form
L. S. D. Morley
(
1955
)
Tests at high subsonic speeds on a 10 per cent thick pressure-plotting aerofoil of RAE 104 section
E. W. E. Rogers
;
C. J. Berry
;
R. F. Cash
(
1951
)
Air-cooling methods for gas-turbine combustion systems
F. J. Bayley
(
1951
)
Secondary flow and losses in a compressor cascade
Jean F. Louis
(
1958
)
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
)
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