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Aeronautical Research Council: Recent submissions
Now showing items 2621-2640 of 2786
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Report of the third year's flying on the development of flight testing techniques for finding and measuring natural icing conditions
G. C. Abel
(
1956
)
Report of the first year's flying on the development of flight testing techniques for finding and measuring natural icing conditions
G. C. Abel
(
1956
)
The effect of lacing wire on axial compressor stage performance at low speeds
S. J. Andrews
;
H. Ogden
(
1956
)
Report of the second year's flying on the development of flight testing techniques for finding and measuring natural icing conditions
G. C. Abel
(
1956
)
A corrected speed tachoscope
R. Staniforth
(
1956
)
Wind tunnel tests on a 6 ft diameter helicopter rotor
T. B. Owen
;
R. Fail
;
R. C. W. Eyre
(
1955
)
An Investigation of High Altitude Cruising Conditions for Turbo-jet Aircraft
R. T. Shields
;
J. Stephenson
;
I. E. Utting
(
1956
)
On the laminar boundary layer separation from the leading edge of a thin aerofoil
P. R. Owen
;
L. Klanfer
(
1955
)
Methods for reducing seaplane take-off distances to standard conditions
J. A. Hamilton
(
1955
)
The torsional vibrations of a class of thin, tapered, solid wings
Elizabeth A. Frost
(
1955
)
Stress considerations in the design of pressurised shells
E. H. Mansfield
(
1955
)
Optical characteristics of laminated camera windows
A.C. Marchant
;
B.M. Mathieson
(
1955
)
Pressure distributions illustrating flow reattachment behind a forward mounted flap
E.C. Maskell
(
1955
)
The laminar boundary-layer with distributed suction on an infinite yawed cylinder
K. D. P. Sinha
(
1955
)
Methods of determination and of fixing boundary layer transition on wind tunnel models at supersonic speeds
K. G. Winter
;
J. B. Scott-Wilson
;
F. V. Davies
(
1955
)
Pressure distributions: axially symmetric bodies in oblique flow
I. J. Campbell
;
R.G. Lewis
(
1955
)
Further experiments with a slotted-wall test section
F. Vandrey
(
1955
)
Investigation of high length/beam ratio seaplane hulls with high beam loadings hydrodynamic stability part 10 the effect of afterbody length on stability and spray characteristics
D.M. Ridland
(
1955
)
An analysis of aerodynamic data on blowing over trailing edge flaps for increasing lift
J. Williams
(
1955
)
Full scale measurements of impact loads on a large flying boat (sunderland Mk.5) part 2 results for impacts on main step
J. A. Hamilton
(
1951
)
Now showing items 2621-2640 of 2786
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