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Showing 10 out of a total of 460 results for collection: Aeronautical Research Council Reports & Memoranda.
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Estimation of the change in performance characteristics of a turbine resulting from changes in the gas thermodynamic properties
D. G. Ainley
(
1951
)
Wind-tunnel flutter tests on a model delta wing under fixed and free root conditions
D. R. Gaukroger
;
E. W. Chapple
;
A. Milln
(
1950
)
Further results on the mixing of free axially-symmetrical jets of mach number 1.40
N. H. Johannesen
(
1959
)
A detailed experimental comparison of axial compressor blades designed for free vortex flow and equivalent untwisted and twisted constant section blades
S. J. Andrews
;
H. Ogden
(
1953
)
Heat transfer and laminar-boundary-layer separation in steady compressible flow past a wall with non-uniform temperature
N. Curle
(
1958
)
Numerical methods for calculating the zero-lift wave drag and the lift-dependent wave drag of slender wings
J. Weber
(
1959
)
High-speed wind-tunnel tests on six wings of 40-deg sweepback, with various section shapes
L. N. Holmes
;
A. B. Haines
(
1952
)
Use of camber and twist to produce low-drag delta or swept-back wings, without leading-edge singularities, at supersonic speeds
G. M. Roper
(
1958
)
A method of performance estimation for axial-flow turbines
D. G. Ainley
;
G. C. R. Mathieson
(
1951
)
Boundary-layer measurements on 15-deg and 24.5-deg cones at small angles of incidence at M = 3.17 and 3.82 and zero heat transfer
F. V. Davies
;
R. J. Monaghan
(
1957
)
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J. Weber (13)
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