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Showing 10 out of a total of 460 results for collection: Aeronautical Research Council Reports & Memoranda.
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An approximate method of calculating the laminar boundary layer in two-dimensional incompressible flow
M. R. Head
(
1957
)
Some flutter tests on swept-back wings using ground-launched rockets
W. G. Molyneux
;
F. Ruddlesden
(
1953
)
Gust alleviation factor. Parts I, II and III
J. K. Zbrozek
(
1953
)
Subsonic wind-tunnel tests on a crescent-winged aircraft, including tests of leading-edge droop designs and several tailplane heights
C. N. Hall
;
B. J. Prior
(
1955
)
On axi-symmetrical gas jets, with application to rocket jet flow fields at high altitudes
W. T. Lord
(
1959
)
Measurements of the effect of windscreen shapes on the drag of cockpit canopies at transonic and low supersonic speeds using the free-flight-model technique
C. Kell
(
1954
)
Thermodynamic charts for the combustion products of nitric acid and kerosene
W. H. Williams
(
1950
)
Tests in the Royal Aircraft Establishment 10-ft x 7-ft high-speed tunnel on 50-deg swept-back wings. Part I. Three of 7.5 per cent thickness. Part II. One of 7.5 per cent thickness with stall fences and leading-edge chord extension
A. B. Haines
;
C. W. Rhodes
(
1954
)
Helicopter control to trim in forward flight
W. Stewart
(
1950
)
Measurements of the direct hinge-moment derivatives at subsonic and transonic speeds for a cropped delta wing with oscillating flap
J. B. Bratt
;
C. J. W. Miles
;
R. F. Johnson
(
1957
)
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J. Weber (13)
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