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AERADE: Recent submissions
Now showing items 3181-3200 of 3498
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Some tests in a slotted-wall tunnel with various slot-entry shapes
A. Chinneck
;
N. A. North
(
1958
)
Records of Static Pressure Tests on Pressure Cabins
P. B. Hovell
;
A. R. Butler
(
1958
)
Records are given of the strengths under static pressure of test specimens of twenty different types of pressurised fuselage.
The effect on weather minima of approach speed, cockpit cut-off angle and type of approach coupler for a given landing success rate and level of safety
E. S. Calvert
;
J. W. Sparke
(
1958
)
An analogue computer for convective heating problems
H. G. R. Robinson
(
1957
)
Regularities in creep and hot-fatigue data part 1
A. Graham
;
K. F. A. Walles
(
1958
)
Nozzle and contraction shapes of the R.A.E. 3 ft x 3 ft supersonic wind tunnel
A. Stanbrook
(
1957
)
A simplified form of the auxiliary equation for use in the calculation of turbulent boundary layers
T. J. Black
(
1958
)
Turbulence measurements in supersonic flow with the hot-wire anemometer
B. Wise
;
D. L. Schultz
(
1957
)
A note on some integrals in aerodynamics
D.E. Williams
(
1957
)
Fatigue loadings in flight - loads in the tailplane of a comet 1
Anne Burns
(
1957
)
A geared flywheel balance arrangement for the prevention of control surface flutter
W. G. Molyneux
(
1957
)
Some proposals regarding the definitions of terms relating to various flow regimes of a gas
C. H. E. Warren
;
A. D. Young
(
1958
)
Experimental investigation of the pressure distribution at the centre-section of a sweptback wing at high subsonic speeds
T. E. B. Bateman
;
A. J. Lawrence
(
1957
)
Report of the definitions panel on definitions to be used in the description and analysis of drag
Aeronautical Research Council
(
1958
)
Experimental correlation between the endurance of a wing spar joint and the ratio between 0.1 percent proof and ultimate tensile strengths of the material
W.A.P. Fisher
(
1958
)
Assessment of the possibility of using suction to inhibit cavitation on cylindrical sections
G. E. Thomas
(
1957
)
Formulae and approximations for aerodynamic heating rates in high speed flight
R. J. Monaghan
(
1957
)
The calculation of the paths of vortices from a system of vortex generators, and a comparison with experiment
J. P. Jones
(
1957
)
Ultrasonic relaxation and attenuation in freons, in relation to their use in supersonic wind tunnels
Y. Miyahara
;
E. G. Richardson
(
1957
)
Curves suitable for families of aerofoils with variable maximum thickness position, nose radius, camber and nose droop
L. H. tanner
(
1957
)
Now showing items 3181-3200 of 3498
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