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Aeronautical Research Council: Recent submissions
Now showing items 1521-1540 of 2786
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An assessment of the accuracy of subsonic linearized theory for the design of warped slender wings
Patricia J. Davies
(
1975
)
Low-speed wind-tunnel tests of a two-dimensional wing fitted with two plain differentially-deflected trailing-edge flaps
John Mckie
(
1975
)
Systems of coordinates suitable for the numerical calculation of three-dimensional flow fields
K. W. Mangler
;
J. C. Murray
(
1975
)
A non-axisymmetric end-wall boundary-layer theory for axial compressor rows
J.W. Railly
(
1975
)
Developments in the lifting surface theory treatment of symmetric planforms with a leading edge crank in subsonic flow
B.L. Hewitt
;
W. Kellaway
(
1975
)
The theory of partial retraction of imperfectly elastic ropes
G.W.H. Stevens
(
1975
)
A theoretical and experimental investigation of the external-flow, jet-augmented flap
P. R. Ashill
(
1975
)
The characteristics of a family of rooftop aerofoils designed at their drag-rise condition in viscous, compressible flow part 1 design condition
B. G. J. Thompson
;
S. W. Cosby
(
1975
)
Measurements of oscillatory aerodynamic hinge moments from the response of a wind tunnel model to turbulent flow
G. B. Hutton
;
D. A. Drane
;
D. R. Gaukroger
(
1975
)
Observations of the flow from a rectangular nozzle
A. G. Kurn
(
1975
)
Free-flight model dynamic stability measurements on a 'not-so-slender' wing/fin combination at zero and small lift, M = 0.8 to 2.0
G. H. Greenwood
;
Geraldine F. Edwards
(
1975
)
The characteristics of a family of rooftop aerofoils designed at their drag-rise condition in viscous, compressible flow part 2 off design conditions
B. G. J. Thompson
;
S. W. Cosby
(
1975
)
The effect of load dwells during fatigue crack propagation
F. E. Kiddle
(
1975
)
Fatigue crack propagation in thin sheets of L73 under constant strain amplitude
P. H. O'Neill
(
1975
)
The dynamic stability derivatives of a slender wing at zero and moderate lift a comparison of theory with free-flight model tests, M 0.8 to 2.0
A. Jean Ross
;
Geraldine F. Edwards
;
A. P. Waterfall
(
1975
)
A finite-difference scheme for computing supercritical flows in arbitrary coordinate systems
C. M. Albone
(
1975
)
The prediction of boundary-layer behaviour and profile drag for infinite yawed wings part 3 calculations for a particular wing
B. G. J. Thompson
;
G. A. Carr-Hill
;
M. Ralph
(
1974
)
An investigation into the duty cycle of powered flying controls parts 1 and 2
F. Holoubek
(
1975
)
Thrust/drag analysis for a front fan nacelle having two separate co-axial exhaust streams
P. G. Street
(
1975
)
The prediction of boundary-layer behaviour and profile drag for infinite yawed wings part 2 flow near a turbulent attachment line
B. G. J. Thompson
(
1974
)
Now showing items 1521-1540 of 2786
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