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Showing 9 out of a total of 39 results for collection: Aeronautical Research Council Reports & Memoranda.
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An approximate integral method for calculating the incompressible laminar boundary layer on an infinite swept wing on which velocity and suction distribution are arbitrary
H. G. Pinsent
;
P. A. Pinsent
(
1959
)
Part I. A Description of the Excitation and Recording Equipment used for Flight Flutter Tests on a Meteor 8. Part II. Comparative Flight Flutter Tests using the 'Decaying Oscillation' and 'Amplitude Response' Techniques
P. D. R. Luscombe
;
W. T. Kirkby
(
1959
)
A wind-tunnel investigation of the directional and longitudinal stability of the Javelin aircraft at transonic speeds, including comparison with flight test results
E. P. Sutton
;
A. Stanbrook
(
1959
)
Wind tunnel tests and theoretical investigations on the effect of a localised mass on the flutter of a delta wing with fixed root
G. F. Donno
(
1959
)
Some possible effects of transonic speeds on wing-aileron flutter
E. G. Broadbent
;
E. Violet Hartley
(
1959
)
The performance of supersonic turbine nozzles
B. S. Stratford
;
G. E. Sansome
(
1959
)
Formulae for calculating the camber surfaces of thin swept-back wings of arbitrary plan-form with subsonic leading edges, and specified load distribution
G. M. Roper
(
1959
)
The buckling of a pressurised stiffened cylinder under axial load
K. I. McKenzie
(
1959
)
The test performance of highly loaded turbine stages designed for high pressure ratio
I. H. Johnston
;
D. C. Dransfield
(
1959
)
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W. T. Lord (3)
B. S. Stratford (2)
J. C. Cooke (2)
J. Weber (2)
P. Bradshaw (2)
W. E. A. Acum (2)
A. Stanbrook (1)
B. D. Henshall (1)
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Date Issued
1959 (39)