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AERADE: Recent submissions
Now showing items 2961-2980 of 3498
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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
)
Subjective response to sonic bangs
M. J. Clarke
;
J. F. Wilby
(
1962
)
Observations of Stall Cells in a Single Stage Compressor
J. Durham
(
1962
)
A specially developed pressure-measuring instrument has been used to observe instantaneous values of the pressure, velocity and direction of the flow in a single stage, low hub-tip ratio, axial compressor. During stall ...
Surface oil-flow patterns on wings of different leading-edge radius and sweepback
H. C. Garner
;
D. K. Cox
(
1961
)
Gusts at low altitude in North Africa
N. I. Bullen
(
1962
)
An amplitude probability analyser for use in turbulence and noise measurements
R. F. Johnson
(
1962
)
Wind tunnel tests at Mach numbers between 0.6 and 1.4 of a 60 degrees swept wing having an aerofoil section designed for subcritical flow at a Mach number of 1.2 part 1 9 percent thick section with "triangular" pressure distribution
E. F. Lawlor
(
1962
)
A survey of buffeting loads
Diana M. Seal
(
1959
)
An investigation into the effects of ground proximity on twin coaxial annular jets, using hotand cold air
R. V. Barrett
;
J. C. Tipping
(
1960
)
Now showing items 2961-2980 of 3498
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