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Showing 10 out of a total of 636 results for collection: Aeronautical Research Council Current Papers.
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A simple flexible supersonic wind tunnel nozzle for the rapid and accurate variation of flow mach number
D. Pierce
(
1967
)
Low-speed wind-tunnel tests on a delta-wing aircraft model (S.R. 177), with blowing over the trailing-edge flaps and ailerons
S. F. J. Butler
;
M. B. Guyett
(
1966
)
Wind tunnel measurements of normal force and pitching moment at a mach number of 2.00 on a 1:30 scale model of blue streak
E. Huntley
(
1964
)
A turbine nozzle cascade for cooling studies part 1 the measurement of mean nusselt numbers at the blade surface
R. I. Hodge
(
1960
)
Measurements of vortex-breakdown position at low speed on a series of sharp-edged symmetrical models
P. B. Earnshaw
(
1965
)
Measurements of the rolling response of a fighter aeroplane (hunter MK.6) to turbulent air and a comparison with theory
J. Burnham
(
1966
)
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
)
Atmospheric turbulence and aircraft height-keeping accuracy
B. A. M. Piggott
(
1967
)
The comparison of theory and experiment for oscillating wings
W. E. A. Acum
(
1963
)
The chemical contouring of 3 percent chromium-molybdenum-vanadium and 5 percent chromium-molybdenum-vanadium high strength steel sheet
Bristol Aerojet Ltd
(
1965
)
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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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