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AERADE: Recent submissions
Now showing items 2761-2780 of 3498
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Wind tunnel tests at mach numbers up to 1.8 on a model with .03 scale wings and nacelles of a twin-engined supersonic aircraft (Bristol 188)
E.P. Sutton
;
P.G. Hutton
;
L.C. Squire
(
1965
)
The design and development of an air-bearing for the measurement of damping in yaw on a jet-blowing model
A. P. Cox
(
1965
)
The calculation of aircraft motion in design rolling manoeuvres
D. J. Eckford
(
1965
)
Pressure distribution measurements on a series of slender delta body shapes at mach numbers of 6.85 and 8.60
D. H. Peckham
(
1965
)
A comparison of rivet shear strengths obtained from two-rivet specimens and from multi-rivet specimens at room temperature and 150 degrees C
D. F. Wright
;
P. Judson
;
P. W. Horrocks
(
1965
)
Aircraft vortex wakes and their effects on aircraft
R. Rose
;
F. W. Dee
(
1965
)
A semi-empirical prediction method for pressures on the windward surface of circular cones at incidence at high supersonic and hypersonic speeds (M is greater than or equal to 3)
J. R. Collingbourne
;
L. F. Crabtree
;
W. J. Bartlett
(
1965
)
The mixing between hot and cold airstreams in a centrifugal field
B. S. Stratford
;
Z. M. Jawor
;
Maureen M. Smith
(
1965
)
Proposals for an integrated wind tunnel-flight dynamics simulator system
L.J. Beecham
;
W.L. Walters
;
D.W. Partridge
(
1965
)
Effect on the static strength of aluminium alloy test specimens of the attachment of thermocouples by a welding technique
D. F. Wright
;
G. F. Acheson
(
1965
)
Effects of varied loading paths on fatigue endurances part 1 some load fatigue properties of nimonic 90 at elevated temperatures
G. P. Tilly
(
1965
)
Mach number distributions along the slotted walls of the N.P.L. 20 in. x 8 in. high-speed wind tunnel
H. H. Pearcey
;
J. D. Regan
(
1965
)
Atmospheric turbulence encountered by Hermes aircraft on routes to Africa and the Far East
Judy E. Aplin
(
1965
)
Effects of varied loading paths on fatigue endurances part 2 some load fatigue properties of H46 at room temperature
G. P. Tilly
(
1965
)
The change of pitot pressure across oblique shock waves in a perfect gas
W. J. Graham
;
B. M. Davis
(
1965
)
Effects of varied loading paths on fatigue endurances part 3 some stress fatigue properties of H46 at elevated temperatures
G. P. Tilly
(
1965
)
The pressure distribution at zero-lift on some slender delta wings at supersonic speeds
M. C. P. Firmin
(
1964
)
Effect of flow curvature due to the fuselage on the flapping motion of a helicopter rotor
M. A. P. Willmer
(
1965
)
A simple method of calculating the flow produced in an annular electric arc heater
J. M. Shaw
(
1965
)
Wind tunnel tests between M = 0.4 and 2.0 on a cambered wing of slender ogee planform
M. D. Dobson
;
R. King-Underwood
(
1965
)
Now showing items 2761-2780 of 3498
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