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Showing 10 out of a total of 367 results for collection: Aeronautical Research Council Reports & Memoranda.
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Calculation of stability derivatives for tapered wings of hexagonal planform oscillating in a supersonic stream
Doris E. Lehrian
(
1960
)
A Theory of the Blockage Effects on Bluff Bodies and Stalled Wings in a Closed Wind Tunnel
E. C. Maskell
(
1963
)
An experimental investigation into the behaviour of the turbulent boundary layers with distributed suction in regions of adverse pressure gradient
B. G. J. Thompson
(
1969
)
On the vibrations of cylindrically curved elastic sandwich plates part 1 with the solution for flat plates part 2 the solution for cylindrical plates
D. J. Mead
;
A. J. Pretlove
(
1962
)
Measurements, at mach numbers up to 2.8, of the longitudinal characteristics of one plane and three cambered slender 'ogee' wings
C. R. Taylor
(
1961
)
Flight tests to investigate the dynamic lateral-stability characteristics of a 45-deg delta, cropped to give three aspect ratios
J. E. Nethaway
;
J. Clark
(
1960
)
An experimental investigation of wind-tunnel wall conditions for interference-free dynamic measurements
A. W. Moore
;
K. C. Wight
(
1969
)
The analysis of blade vibration due to random excitation
D. S. Whitehead
(
1960
)
The flow produced by interaction of a turbulent boundary layer with a normal shock wave of strength sufficient to cause separation
J. Seddon
(
1960
)
An application of the R.A.E. wind-tunnel/flight dynamics simulator to the low-speed dynamics of a slender delta aircraft (HP 115)
D. W. Partridge
;
B. E. Pecover
(
1969
)
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E. W. E. Rogers (9)
H. C. Garner (8)
C. J. Berry (7)
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W. J. G. Pinsker (7)
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