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Showing 10 out of a total of 14 results for community: Aeronautical Research Council (1945-1979).
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The calculation of the velocity distribution due to thickness for swept wings with subsonic edges at supersonic speeds
A. B. Haines
;
K. Rollins
;
J. Osborn
(
1962
)
A comparison of results in the A.R.A. transonic tunnel on a small and a large model of a slender wing
T. E. B. Bateman
;
A. B. Haines
(
1961
)
The effect of leading-edge geometry on high-speed stalling
G. F. Moss
;
A. B. Haines
;
R. Jordan
(
1973
)
Afterbody drag measurement at transonic speeds on a series of twin and single jet afterbodies terminating at the jet-exit
O. M. Pozniak
;
A. B. Haines
(
1973
)
Pressure plotting tests in the Royal Aircraft Establishment high speed wind tunnel on a 21 per cent thick, low drag aerofoil (Brabazon 1 wing root section)
A. B. Haines
;
W. Port
(
1947
)
High-speed wind-tunnel tests on six wings of 40-deg sweepback, with various section shapes
L. N. Holmes
;
A. B. Haines
(
1952
)
Some notes on the flow patterns observed over various swept-back wings at low Mach numbers (in the R.A.E. 10-ft x 7-ft high speed tunnel)
A. B. Haines
(
1954
)
The centre-line mach-number distributions and auxiliary-suction requirements for the A.R.A. 9-ft X 8-ft transonic wind tunnel
A. B. Haines
;
J. C. M. Jones
(
1958
)
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
)
Aerodynamic loads on external stores a review of experimental data and method of prediction
P. Marsden
;
A. B. Haines
(
1962
)
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A. B. Haines (14)
T. E. B. Bateman (2)
A. R. C. MacDougall (1)
C. W. Rhodes (1)
D. E. Hartley (1)
G. C. Browne (1)
G. F. Moss (1)
J. C. M. Jones (1)
J. Osborn (1)
K. Rollins (1)
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Date Issued
1970 - 1973 (3)
1960 - 1969 (3)
1950 - 1959 (5)
1946 - 1949 (3)