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Aeronautical Research Council: Recent submissions
Now showing items 1941-1960 of 2786
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Stiffness, damping and creep properties of a polyurethane foam including the effects of temperature and humidity
D. B. Payen
(
1967
)
A preliminary flight simulation study of jet-borne V.T.O.L. aircraft handling qualities
D. H. Perry
;
H. W. Chinn
(
1967
)
A flight simulation study of difficulties in piloting large jet transport aircraft through severe atmospheric disturbances
D. H. Perry
;
J. Burnham
(
1967
)
Balance measurements (excluding drag) on a delta wing aircraft at transonic speeds
M. M. Shaw
(
1967
)
Wind tunnel measurements of the effect of a jet on the time average and unsteady pressures on the base of a bluff afterbody
J.E. Rossiter
;
A.G. Kurn
(
1967
)
The spectral energy balance in a turbulent mixing layer
P. Bradshaw
;
D. H. Ferriss
(
1967
)
Crack propagation in fatigue. Some experiments with DTD 5070A aluminium alloy sheet
D. P. Rooke et al
(
1967
)
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
)
Now showing items 1941-1960 of 2786
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