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Aeronautical Research Council: Recent submissions
Now showing items 2461-2480 of 2786
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Calculation of the shape of a thin slender wing for a given load distribution and planform
J. H. B. Smith
(
1958
)
The geometry of wing surfaces generated by straight lines and with a high rate of thickness taper at the root
D. Peckham
(
1958
)
The calibration at transonic speeds of a mark 9A pitot static head with and without flow through the static slots
D. G. Mabey
(
1958
)
Tables of aerodynamic flutter derivatives for thin wings and control surfaces in two dimensional supersonic flow
I. T. Minhinnick
;
D. L. Woodcock
(
1958
)
Regularities in creep and hot-fatigue data part 2
K. F. A. Walles
;
A. Graham
(
1958
)
Measurements of the effect of surface cooling on boundary layer transition on a 15 degrees cone part 1 tests at M = 2 and 3 in an 8 in. x 9 in. wind tunnel at R.A.E./Bedford
A. C. Browning
;
J. F. W. Crane
;
R. J. Monaghan
(
1958
)
Flutter prediction in practice
E. G. Broadbent
(
1957
)
Tests on a two-dimensional slotted-wall wind tunnel with lateral obstructions behind the slots
A. Chinneck
;
C. J. Berry
;
P. J. Peggs
(
1958
)
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
)
Now showing items 2461-2480 of 2786
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