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Showing 10 out of a total of 367 results for collection: Aeronautical Research Council Reports & Memoranda.
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A review of research on two-dimensional base flow
J. F. Nash
(
1962
)
Wind tunnel tests of a wing fitted with a single lifting fan
N. Gregory
;
W. G. Raymer
;
Edna M. Love
(
1964
)
Flight measurements of the lift, longitudinal trim and drag of the fairey delta 2 at mach numbers up to 1.65 and comparisons with wind-tunnel results
R. Rose
;
C. S. Barnes
;
A. A. Woodfield
(
1967
)
Feed-back accelerometer circuits with a velocity output
R. H. Evans
;
G. G. Haigh
(
1964
)
Measurement of skin friction at low subsonic speeds by the razor-blade technique
L. F. East
(
1966
)
Tables of supersonic symmetrical flow around right circular cones, with and without the addition of heat at the wave
R. S. Bartlett
(
1966
)
An investigation of the flow about a plane half-wing of cropped-delta planform and 6 per cent symmetrical section at stream mach numbers between 0.8 and 1.41
E. W. E. Rogers
;
I. M. Hall
;
C. J. Berry
(
1960
)
Leakage and secondary flows i compressor cascades
B. Lakshminarayana
;
J. H. Horlock
(
1965
)
Upwash interference on wings of finite span in a rectangular wind tunnel with closed side walls and porous-slotted floor and roof
D. R. Holder
(
1963
)
Variable stability and control tests on the S.C.1 aircraft in jet-borne flight, with particular reference to desirable VTOL flying qualities
J. K. B. Illingworth
;
H. W. Chinn
(
1963
)
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E. W. E. Rogers (9)
H. C. Garner (8)
C. J. Berry (7)
D. E. Davies (7)
W. J. G. Pinsker (7)
D. S. Whitehead (6)
Doris E. Lehrian (6)
G. G. Pope (6)
P. Bradshaw (6)
A. J. Sobey (5)
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1964 (37)
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