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Aeronautical Research Council Current Papers: Recent submissions
Now showing items 1241-1260 of 1393
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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
)
Experiments on a slotted-wall working section in a wind tunnel
F. Vandrey
;
K. Wieghardt
(
1955
)
Theory of the broad-bladed propeller
G. I. Ginzel
(
1955
)
Investigation of high length/beam ratio seaplane hulls with high beam loadings hydrodynamic stability part 6 the effect of forebody warp on stability and spray characteristics
D. M. Ridland
(
1955
)
List of current papers published by the Aeronautical Research Council (numbers 151-200)
Aeronautical Research Council
(
1955
)
Investigation of high length/beam ratio seaplane hulls with high beam loadings hydrodynamic stability part 2 the effect of changes in the mass, moment of inertia and radius of gyration on longitudinal stability limits
J. K. Friswell
;
A. Kurn
;
D.M. Ridland
(
1955
)
Investigation of high length/beam ratio seaplane hulls with high beam loadings hydrodynamic stability part 1 techniques and presentation of results of model tests
D. M. Ridland
;
J. K. Friswell
;
A. G. Kurn
(
1955
)
Some notes on the calculation of pressure pick-up sensitivity and the conditions for maximum sensitivity and the development of a miniature pressure pick-up
J. K. Friswell
(
1955
)
Requirements for uniformity of flow in supersonic wind tunnels
D. E. Morris
;
K. G. Winter
(
1955
)
A criterion for the prediction of the recovery characteristics of spinning aircraft
T. H. Kerr
(
1955
)
A note on the sound from weak disturbances of a normal shock wave
Alan Powell
(
1955
)
Tests on a swept-back wing and body with endplates and wing tip tanks in the compressed air tunnel
C. Salter
;
R. Jones
(
1954
)
Wide range amplifier for turbulence measurements with adjustable upper frequency limit
H. Schuh
;
D. Walker
(
1955
)
Some visual observations of the flow over a swept-back wing in a water tunnel, with particular reference to high incidences
M. C. Lambourne
;
P. S. Pusey
(
1955
)
Now showing items 1241-1260 of 1393
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