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Aeronautical Research Council: Recent submissions
Now showing items 2041-2060 of 2786
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On the calculation of cascade flows
W. S. Hall
;
B. Thwaites
(
1965
)
Tests with a variable ramp intake having combined external/internal compression, and a design mach number of 2.2
M. C. Neale
;
P. S. Lamb
(
1965
)
Wind tunnel measurements of the far-field pressures due to some lifting, slender delta wings
T. A. Cook
(
1965
)
An experimental investigation into the determination of lift from wake traverses at supersonic speeds
J. Wooller
;
M.C.P. Firmin
(
1965
)
List of current papers (numbers 751-800)
Aeronautical Research Council
(
1965
)
Wind tunnel tests at mach numbers up to 2.80 to determine the effects of changing spanwise volume distribution on a slender, cambered ogee wing
T. A. Cook
(
1965
)
Wind tunnel measurements at mach numbers up to 2.80 of the effects of gulling on the longitudinal and lateral stability and drag of a cambered, slender ogee wing
T. A. Cook
(
1965
)
The steady flow of a viscous fluid past a circular cylinder
S. C. R. Dennis
;
M. Shimshoni
(
1965
)
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
)
Now showing items 2041-2060 of 2786
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