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AERADE: Recent submissions
Now showing items 2661-2680 of 3498
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A survey of unsteady hypersonic flow problems
B. M. Wood
(
1966
)
Measurements of the rolling response of a fighter aeroplane (hunter MK.6) to turbulent air and a comparison with theory
J. Burnham
(
1966
)
The effect of external flow on an internal-expansion propelling nozzle incorporating ventilation by ambient air
M. V. Herbert et al
(
1966
)
List of current papers (numbers 851-900)
Aeronautical Research Council
(
1967
)
Notes on Ducted Fan Design
R. C. Turner
(
1964
)
In general, conventional compressor stages are designed by the cascade method, while high stagger low solidity ducted fans are designed on modified isolated aerofoil theory. The purpose of these notes is to provide a basis ...
An experimental investigation of the influence of base bleed on the base drag of various propelling nozzle configurations
J. B. Roberts
;
G. T. Golesworthy
(
1966
)
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
)
Now showing items 2661-2680 of 3498
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