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Aeronautical Research Council: Recent submissions
Now showing items 2261-2280 of 2786
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Subjective response to sonic bangs
M. J. Clarke
;
J. F. Wilby
(
1962
)
Observations of Stall Cells in a Single Stage Compressor
J. Durham
(
1962
)
A specially developed pressure-measuring instrument has been used to observe instantaneous values of the pressure, velocity and direction of the flow in a single stage, low hub-tip ratio, axial compressor. During stall ...
Surface oil-flow patterns on wings of different leading-edge radius and sweepback
H. C. Garner
;
D. K. Cox
(
1961
)
Gusts at low altitude in North Africa
N. I. Bullen
(
1962
)
An amplitude probability analyser for use in turbulence and noise measurements
R. F. Johnson
(
1962
)
Wind tunnel tests at Mach numbers between 0.6 and 1.4 of a 60 degrees swept wing having an aerofoil section designed for subcritical flow at a Mach number of 1.2 part 1 9 percent thick section with "triangular" pressure distribution
E. F. Lawlor
(
1962
)
A survey of buffeting loads
Diana M. Seal
(
1959
)
An investigation into the effects of ground proximity on twin coaxial annular jets, using hotand cold air
R. V. Barrett
;
J. C. Tipping
(
1960
)
The design and testing of a low range acceleration transducer with predictable response characteristics
I. McLaren
(
1961
)
Scale models for thermo-aeroelastic research
W. G. Molyneux
(
1961
)
Low-speed pressure-plotting tests on a flat-plate m-wing fitted with part-span nose-flaps
L.A. Wyatt
;
G.P. Ilott
(
1961
)
Low-speed wind-tunnel tests on sharp-edged gothic wings of aspect-ratio .75
R. F. A. Keating
(
1961
)
Turbulence encountered by ambassador aircraft over Europe
J. R. Heath-Smith
(
1960
)
A method of detecting the fully cooled state of a liquid oxygen pipeline
N. Shufflebotham
(
1960
)
Free-flight measurements of control effectiveness on three wing planforms at transonic speeds
J. B. W. Edwards
(
1961
)
Low-speed wind tunnel tests on the effects of taper on low aspect-ratio wings at zero incidence
D. H. Peckham
(
1961
)
The analysis of complex vibrations with spada
S. L. Entres
(
1961
)
An experimental study of the drag of rigid models representing two parachute designs at M = 1.40 and 2.19
B. G. Roberts
(
1961
)
Note on the time required for the achievement of steady flow past a slender body in a hypersonic shock tunnel
D. W. Holder
;
D. L. Schultz
(
1961
)
A note on the effects of heat transfer on the separation of a laminar boundary layer
G. E. Gadd
;
J. L. Attridge
(
1961
)
Now showing items 2261-2280 of 2786
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