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Showing 10 out of a total of 460 results for collection: Aeronautical Research Council Reports & Memoranda.
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Heat-transfer and skin-friction measurements at a mach number of 2.44 for a turbulent boundary layer on a flat surface and in regions of separated flow
G. E. Gadd
;
W. F. Cope
;
J. L. Attridge
(
1958
)
The geared elevator tab and tail-unit stiffness requirements
T. Niblett
(
1951
)
Measurements of two-dimensional derivatives on a wing-aileron-tab system with a 1541 section aerofoil. Part 1 direct aileron derivatives
K. C. Wight
(
1952
)
Published reports and memoranda of the aeronautical research council
Aeronautical Research Council
(
1958
)
A simple method for calculating the span and chordwise loading on straight and swept wings of any given aspect ratio at subsonic speeds
D. Küchemann
(
1952
)
Charts of peak amplitudes in incidence and sideslip in rolling manoeuvres due to inertia cross coupling
W. J. G. Pinsker
(
1958
)
An experimental investigation at supersonic speeds of the characteristics of two gothic wings, one plane and one cambered
L. C. Squire
(
1959
)
The calculation of the compressible turbulent boundary layer in an arbitrary pressure gradient a correlation of certain previous methods
B. S. Stratford
;
G. S. Beavers
(
1959
)
An experimental investigation of leading-edge flow separation from a 4 per cent thick two-dimensional biconvex aerofoil
B. D. Henshall
;
R. F. Cash
(
1957
)
Water and air performance of seaplane hulls as affected by fairing and fineness ratio
A. G. Smith
;
J. E. Allen
(
1950
)
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