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Showing 10 out of a total of 636 results for collection: Aeronautical Research Council Current Papers.
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Free-flight measurements of pressure and heat transfer in regions of separated and reattached flow at mach numbers up to 4
J. Picken
(
1965
)
The evaluation of some commercial and development pressure gauges in a laboratory type shock tube with a view to their suitability for use in shock tunnels
D. R. Stevens
(
1962
)
Low-speed wind tunnel tests on the effects of taper on low aspect-ratio wings at zero incidence
D. H. Peckham
(
1961
)
Trials of an experimental low airspeed indicator for helicopters
Staff of Airborne
;
Helicopter Division
;
ARC
(
1961
)
Wind tunnel tests at mach numbers up to 2.80 to determine the effects of changing spanwise volume distribution on a slender, cambered ogee wing
T. A. Cook
(
1965
)
The time required for high speed airstreams to disintegrate water drops
D. C. Jenkins
;
J. D. Booker
(
1965
)
Flight and tunnel measurements of pressure fluctuations on the upper surface of the wing of a Venom aircraft with a sharpened leading-edge
R. Rose
;
O. P. Nicholas
(
1967
)
Measurements of transient pressures on a narrow-delta wing due to an upward gust
G. K. Hunt
;
D. R. Roberts
;
D. Walker
(
1964
)
Calculations of the lift slope and aerodynamic centre of cropped delta wings at supersonic speeds
J. H. B. Smith
;
J. A. Beasley
;
A. Stevens
(
1960
)
The measured response of an aircraft to the vertical velocity component of atmospheric turbulence
D. M. Ridland
(
1964
)
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Aeronautical Research Council (17)
D. H. Peckham (8)
J. C. Cooke (8)
G. T. Golesworthy (7)
L. Davies (7)
M. C. Neale (7)
D. G. Mabey (6)
G. K. Hunt (6)
J. F. Nash (6)
N. I. Bullen (6)
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1969 (18)
1968 (66)
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1965 (80)
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