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Aeronautical Research Council Current Papers: Recent submissions
Now showing items 1301-1320 of 1393
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Note on the effect of thickness and aspect ratio on the damping of pitching oscillations of rectangular wings moving at supersonic speeds
W. E. A. Acum
(
1954
)
List of current papers published by the Aeronautical Research Council numbers 101-150
Unknown author
(
1954
)
This paper lists fifty titles which have been published in the CP Series of the Aeronautical Research Council.
Factors influencing the optimum aerodynamic design of cooled turbines
G. F. C. Rogers
(
1954
)
Experiments at M = 1.8 on bodies of revolution having ogival heads
H. K. Zienkiewicz et al
(
1954
)
Vibration and flutter of aircraft aerials
W. H. Johnson
(
1954
)
The Performance of the 108 Compressor Fitted with Low Stagger Free Vortex Blading
D. V. Foster
(
1954
)
Zero lift drag measurements on swept wings at transonic and supersonic speeds using the ground-launched rocket-boosted model technique
T. Lawrence
;
C. Kell
(
1954
)
Theoretical load distributions on wings with cylindrical bodies at the tips
D.E. Hartley
(
1954
)
Unsteady cavitating flow past curved obstacles
L. C. Woods
(
1954
)
A review and assessment of various formulae for turbulent skin friction in compressible flow
R. J. Monaghan
(
1953
)
The measurement of heat transfer and skin friction at supersonic speeds part 3 measurements of overall heat transfer and of the associated boundary layers on a flat plate at Ml = 2.43
R. J. Monaghan
;
J. R. Cooke
(
1953
)
The measurement of heat transfer and skin friction at supersonic speeds part 4 tests on a flat plate at M = 2.82
R. J. Monaghan
;
J. R. Cooke
(
1953
)
An investigation into the pitot rake method of measuring turbo jet engine thrust in flight
J. Stephenson
;
R. T. Shields
;
D. W. Bottle
(
1954
)
The vibrations of a swept wing
N.S. Heaps
(
1953
)
Pressure distribution and boundary layer investigations on 44 degree swept-back tapered wing part 1 three-dimensional tests on the wing part 2 two-dimensional pressure distribution tests on 10 per cent thick symmetrical aerofoil section
Joseph Black
(
1953
)
A relaxation treatment of shock waves
L. C. Woods
(
1953
)
Design of a right-angled bend with constant velocities at the walls
A. S. Thom
(
1953
)
Air cooling methods for gas turbine combustion systems
F. J. Bayley
(
1953
)
Tests on an axial compressor with various stator blade staggers
R.A. Jeffs
;
E.L. Hartley
;
P. Rooker
(
1953
)
The theory of aerofoils with hinged flaps in two-dimensional compressible flow
L. C. Woods
(
1953
)
Now showing items 1301-1320 of 1393
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