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Aeronautical Research Council Current Papers: Recent submissions
Now showing items 561-580 of 1393
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The performance of a centrebody propelling nozzle with a parallel shroud in external flow part 2
M. V. Herbert
;
G. T. Golesworthy
;
R. J. Herd
(
1966
)
The performance of conical convergent-divergent nozzles of area ratios 2.44 and 2.14 in external flow
G. T. Golesworthy
;
J. B. Roberts
;
C. Overy
(
1966
)
The performance of a conical convergent-divergent nozzle with area ratio 2.9 in external flow
G. T. Golesworthy
;
M. V. Herbert
(
1966
)
The use of air injection to prevent separation of the turbulent boundary layer in supersonic flow
D. J. Peake
(
1966
)
Some exploratory tests on a two-dimensional blown-cylinder model in the R.A.E. 2 ft x 1.50 ft transonic-wind tunnel
A. F. Jones
;
W. R. Buckingham
(
1967
)
An experimental investigation of the flow through inclined circular tubes at a mach number of 4.0
P. L. Roe
(
1966
)
A developed theory of spoilers on aerofoils
C. S. Barnes
(
1966
)
A velocity defect relationship for the outer part of equilibrium and near-equilibrium turbulent boundary layers
J. McQuaid
(
1966
)
Plasma flow in an electromagnetic shock tube and in a compression shock tube
J. L. Wilson
;
D. Schofield
;
J. D. Regan
(
1966
)
Aerodynamic study force and moment measurements on three delta wings of aspect ratios 0.83, 1.03 and 1.24 in combination with bodies of fineness ratio 13 at a mach number of 4
D.R. Andrews
(
1966
)
A study on the running times in reflected shock tunnels
J. A. D. Ackroyd
(
1967
)
The interaction of the reflected shock with the boundary layer in a shock tube and its influence on the duration of hot flow in the reflected-shock tunnel part 1
L. Davies
(
1966
)
The interaction of the reflected shock with the boundary layer in a shock tube and its influence on the duration of hot flow in the reflected-shock tunnel part 2
L. Davies
(
1967
)
Bulk compressibility effects in the R.A.R.D.E. no. 3 hypersonic gun tunnel
W. A. Clayden
(
1966
)
On the interaction of the transmitted shock with the boundary layer in a shock tube using argon as test gas
L. Davies
;
K. Bridgman
(
1966
)
Comparison of helicopter and aeroplane vertical accelerations in turbulence
D. A. Webber
(
1966
)
The flapping behaviour of a helicopter rotor at high tip-speed ratios
E. Wilde
;
A. R. S. Bramwell
;
R. Summerscales
(
1966
)
A note on the turbulent uniform-property hydrodynamic boundary layer on a smooth impermeable wall comparisons of theory with experiment
M. P. Escudier
;
D. B. Spalding
(
1966
)
Characteristics of high-speed wind tunnels in the United Kingdom relevant to aeroelastic-model tests
C. A. K. Irwin
(
1967
)
Analysis of hinge moment data for rectangular and near rectangular trailing edge controls at supersonic and transonic speeds
D. Isaacs
(
1966
)
Now showing items 561-580 of 1393
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