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Showing 10 out of a total of 87 results for community: Aeronautical Research Council.
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The aerodynamic derivatives with respect to a rate of yaw for a delta wing with dihedral and at incidence at supersonic speeds
J. H. Hunter-Tod
(
1951
)
Estimation of the change in performance characteristics of a turbine resulting from changes in the gas thermodynamic properties
D. G. Ainley
(
1951
)
A method of performance estimation for axial-flow turbines
D. G. Ainley
;
G. C. R. Mathieson
(
1951
)
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
)
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
)
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
)
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
)
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Author
D. W. Holder (4)
A. Chinneck (3)
A. Spence (3)
D. A. Kirby (3)
D. G. Ainley (3)
D. G. Hurley (3)
R. J. North (3)
W. P. Jones (3)
A. Thom (2)
C. J. Berry (2)
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Date Issued
1951 (87)