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Aeronautical Research Council: Recent submissions
Now showing items 2021-2040 of 2786
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Measurements of vortex-breakdown position at low speed on a series of sharp-edged symmetrical models
P. B. Earnshaw
(
1965
)
Experimental investigation of the breakdown of a vortex in a tube
D. L. I. Kirkpatrick
(
1965
)
A digital recording system for structural research
D. Purslow
(
1965
)
The static pressure distribution around a circular jet exhausting normally from a plane wall into an airstream
L. J. S. Bradbury
;
M. N. Wood
(
1965
)
A parametric study of take-off and landing distances for high-lift aircraft
W. A. Mair
;
B. J. Edwards
(
1965
)
Methods and charts for estimating skin friction drag in wind tunnel tests with zero heat transfer
K. G. Smith
(
1965
)
Analysis of flight loads recorded on comet 4B aircraft by means of the fatigue load meter
R. Hain Taylor
(
1965
)
Measurements of dynamic stability from three simplified free-flight models of a supersonic research aircraft (Bristol T.188) over the mach number range 1.2 - 2.6
K. J. Turner
(
1965
)
Supersonic wind tunnel tests on a 1/12th scale model of the bristol type 188 research aircraft part 1 M = 1.4 to 2.0 part 2 M = 2.0 to 2.7
C. R. Taylor
;
T. A. Cook
(
1965
)
Alleviation of thermal stresses in aircraft structures
E. C. Capey
(
1965
)
Measurements of oscillatory derivatives at mach numbers up to 2.6 on a model of a supersonic transport design study (Bristol type 198)
J. S. Thompson
;
R. A. Fail
(
1965
)
Wind tunnel tests on a 1/12th scale model of the bristol type 188 research aircraft with rectangular, wedge intakes at mach numbers from 2.0 to 2.7
T. A. Cook
(
1965
)
Measurement of air temperature on an aircraft travelling at high subsonic and supersonic speeds
A. A. Woodfield
;
P. J. Haynes
(
1965
)
Measurements of skin-friction in an annulus by the floating element technique
J. K. White
;
R. E. Franklin
(
1965
)
Influence of chemical contouring on the fatigue and sustained load properties of high tensile steel sheet
Westland Aircraft Limited
;
Saunders-Roe Division
(
1965
)
Theoretical investigation of some basic assumptions of Schlichting's singularity method of cascade analysis
R. I. Lewis
;
G. A. Pennington
(
1965
)
The unsteady motion of slender wings with leading-edge vortices
B. D. Dore
(
1965
)
The chemical contouring of 3 percent chromium-molybdenum-vanadium and 5 percent chromium-molybdenum-vanadium high strength steel sheet
Bristol Aerojet Ltd
(
1965
)
Potential flow through cascades extensions to an exact theory
J. P. Gostelow
(
1965
)
Potential flow through cascades a comparison between exact and approximate solutions
J. P. Gostelow
(
1965
)
Now showing items 2021-2040 of 2786
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