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Showing 10 out of a total of 51 results for collection: Aeronautical Research Council Reports & Memoranda.
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The reduction to standard conditions of take-off measurements on turbo-jet aircraft
G. Jackson
;
K. J. Lush
(
1951
)
An analysis of available data on the local aerodynamic centres of aerofoils in two- and three-dimensional flow
A. S. Taylor
(
1951
)
Some applications of the lamé function solutions of the linearised supersonic flow equations. Part I. Finite swept-back wings with symmetrical sections and rounded leading edges. Part II. Cambered and twisted wings
G. M. Roper
(
1951
)
Flutter and resonance characteristics of a model cantilever wing carrying localised masses
N. C. Lambourne
(
1951
)
The geared elevator tab and tail-unit stiffness requirements
T. Niblett
(
1951
)
Experiments on the flow into a swept leading-edge intake at zero forward speed with notes on the wider uses of a slotted intake
J. Seddon
;
W. J. G. Trebble
(
1951
)
An extension of Multhopp's method of calculating the spanwise loading of wing-fuselage combinations
J. Weber
;
D. A. Kirby
;
D. J. Kettle
(
1951
)
Evaporation from the Surface of a Body in an Airstream (With Particular Reference to the Chemical Method of Indicating Boundary-layer Transition)
P. R. Owen
;
A. O. Ormerod
(
1951
)
Experiments with slotted and perforated walls in a two-dimensional high-speed tunnel
D. W. Holder
;
R. J. North
;
A. Chinneck
(
1951
)
Stress concentrations at a cut-out in a swept wing
E. H. Mansfield
(
1951
)
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Author
D. A. Kirby (3)
D. G. Ainley (3)
A. Spence (2)
A. Thom (2)
E. H. Mansfield (2)
G. C. R. Mathieson (2)
J. Seddon (2)
J. Weber (2)
W. J. G. Trebble (2)
W. P. Jones (2)
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Date Issued
1951 (51)