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Aeronautical Research Council: Recent submissions
Now showing items 2241-2260 of 2786
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Minimum energy ballistic trajectories over a non-rotating earth
G. B. Longden
(
1962
)
Some three-dimensional effects of rotating stall
S. L. Dixon
(
1962
)
The calculated effect of the station of maximum cross-sectional area on the wave drag of delta wings
J. H. B. Smith
;
W. Thomson
(
1961
)
Diffraction of a plane straight shock wave
R. S. Srivastava
(
1963
)
The development of the boundary layer in supersonic shear flow
Ruth H. Rogers
(
1962
)
The measurement of absorptivity and reflectivity
E. T. de la Perrelle
;
H. Herbert
(
1956
)
The damping of structural vibrations
G. G. Parfitt
;
D. Lambeth
(
1960
)
Progress report on an experiment on the effect of surface flexibility on the stability of laminar flow
N. Gregory
;
Edna M. Love
(
1961
)
Exploratory wind-tunnel investigations on a bluff body containing a lifting fan
W. J. G. Trebble
;
J. Williams
(
1962
)
The effect of tip bluntness on boundary-layer transition on a 15 degrees included angle cone at M = 3.12 and 3.81
Ruth H. Rogers
(
1962
)
List of current papers published for the Aeronautical Research Council (numbers 551-600)
Aeronautical Research Council
(
1962
)
Comparative calculations of supersonic pitching derivatives over a range of frequency parameter
H. C. Garner
;
W. E. A. Acum
;
Doris E. Lehrian
(
1961
)
A review of the problems of aircraft wheel braking on wet surfaces and a description of a method of artificially wetting runways for test purposes
H. J. Keyes
(
1957
)
Measurements of the pitching moment derivatives for rigid wings of rectangular plan form oscillating about the mid-chord axis in supersonic flow
C. Scruton et al
(
1961
)
Reduction of lift-dependent drag with separated flow
G. H. Lee
(
1959
)
On the control of shock-induced boundary-layer separation with discrete air jets
R. A. Wallis
;
C. M. Stuart
(
1958
)
The 7 in. x 7 in. hypersonic wind tunnel at R.A.E. Farnborough parts 1, 2 and 3
J.F.W. Crane
;
L.F. Crabtree
(
1962
)
An experimental investigation of the characteristics of an ogee wing from M = 0.4 to M = 1.8
L.C. Squire
;
D.S. Capps
(
1962
)
Problems associated with the use of a false wall as a reflection plane for half model tests in the de Havilland high speed wind tunnel
D. R. Holder
;
H. C. Farley
(
1962
)
The estimation of transient temperature distributions and thermal stresses in turbine and compressor discs
M. Cox
(
1961
)
Now showing items 2241-2260 of 2786
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