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Aeronautical Research Council: Recent submissions
Now showing items 2761-2780 of 2786
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A brief survey of some methods and information concerning the aerodynamic derivatives of wings in unsteady motion at transonic and supersonic speeds
W. E. A. Acum
(
1952
)
Wind tunnel tests on a 90 degrees apex delta wing of variable aspect ratio (sweepback 36.8 degrees) part 1 general stability part 2 measurements of downwash and effect of high lift devices
J.G. Ross
;
R. Hills
;
R.C. Lock
(
1952
)
Power requirements for distributed suction for increasing maximum lift
R. C. Pankhurst
;
N. Gregory
(
1952
)
Experiments on distributed suction through a rough porous surface
Cambridge University Aeronautical Laboratory
(
1952
)
N.P.L. Aerofoil catalogue and bibliography
R. C. Pankhurst
(
1952
)
The effects of atmospheric humidity and temperature on the engine power and take-off performance of a hastings 1
G. Jackson
(
1952
)
An experimental investigation of the performance of a pilot plant for drying air by solid granular adsorbents
P.J. Bateman
(
1952
)
High speed wind tunnel tests on an aerofoil with and without two-dimensional spanwise bulges
J. A. Beavan
;
E. W. E. Rogers
;
R. Cartwright
(
1952
)
Calculated Pressure Distributions for the R.A.E. 100-104 Aerofoil Sections
R. C. Pankhurst
;
H. B. Squire
(
1952
)
Approximate two-dimensional aerofoil theory part 4 the design of centre lines
S. Goldstein
(
1952
)
Designing a slot for a given wall velocity
A. Thom
;
Laura Klanfer
(
1952
)
The diffusion of transverse loads in a reinforced circular cylinder with non-rigid frames
S.R. Lewis
(
1952
)
Digital recording and analysing of flight test data a proposed system
E.J. Petherick
(
1952
)
Approximate two-dimensional aerofoil theory part 6 aerofoils with hinged flaps
S. Goldstein
;
J. H. Preston
(
1952
)
Approximate two-dimensional aerofoil theory part 5 the positions of maximum velocity and theoretical CL-ranges
S. Goldstein
(
1952
)
Draft corrections for water surface deflection under no.1 carriage of the R.A.E. seaplane tank
T.B. Owen
(
1952
)
Designing to avoid dangerous behaviour of an aircraft due to the effects on control hinge moments of ice on the leading edge of the fixed surface
D. E. Morris
(
1952
)
Approximate two-dimensional aerofoil theory part 1 velocity distributions for symmetrical aerofoils
S. Goldstein
(
1952
)
Approximate two-dimensional aerofoil theory part 3 approximate designs of symmetrical aerofoils for specified pressure distributions
S. Goldstein
;
E. J. Richards
(
1952
)
Approximate two-dimensional aerofoil theory part 2 velocity distributions for cambered aerofoils
S. Goldstein
(
1952
)
Now showing items 2761-2780 of 2786
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