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Aeronautical Research Council: Recent submissions
Now showing items 2361-2380 of 2786
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Aspects of insect contamination in relation to laminar flow aircraft
I. G. C. Lachmann
(
1960
)
Some tests on cascades of compressor blades fitted with vortex generators
R. Staniforth
(
1960
)
An investigation at transonic speeds of the performance of various distributed rougness bands used to cause boundary-layer transition near the leading edge of a cropped delta half-wing
E.W.E. Rogers et al
(
1960
)
Visualization of secondary flow in the reservoirs of the slotted - wall working sections of the A.R.L. 12-inch and 30-inch water tunnels
D. A. E. Leaver
(
1960
)
The rotating flap as a high-lift device
L. F. Crabtree
(
1960
)
The effect of fuselage modifications on the zero-lift transonic drag of a fighter aircraft (hunter F. Mk.1) as measured by free-flight model tests
G. H. Greenwood
(
1960
)
Some measurements in the vortex flow generated by a sharp leading edge having 65 degrees sweep
N. C. Lambourne
;
D. W. Bryer
(
1960
)
The longitudinal frequency response to elevator of an aircraft over the short period frequency range
D. M. Ridland
(
1960
)
Wind tunnel tests on the flutter of a swept and unswept wing with ailerons
H. Hall
;
J.A. Rein
(
1960
)
Measurements of the effect of surface cooling on boundary layer transition on a 15 degrees cone part 2 tests at M = 3 and M = 4 in the 5 in. x 5 in. no. 5 wind tunnel at R.A.E. Farnborough
J. G. Woodley
(
1960
)
Free-flight experiments on the measurement of free-stream static pressure at transonic speeds with particular reference to the Mk.9 pitot-static head
C. Kell
(
1960
)
Note on conditions for which data on the power spectra at atmospheric turbulence are required
J. K. Zbrozek
;
F. Pasquill
(
1960
)
Some instabilities arising from the interactions between shock waves and boundary layers
N. C. Lambourne
(
1960
)
Fatigue loadings in flight - loads in the tailplane of a devon
Anne Burns
(
1960
)
The centre section shape of swept tapered wings with a linear chordwise load distribution
J.C. Cooke
(
1960
)
An investigation of the flow over a half-wing model with 60.5 degrees leading edge sweepback, at a high subsonic and supersonic speeds
F. O'Hara
;
J. B. Scott-Wilson
(
1960
)
Power spectrum analysis of gust loads on the comet wing and tailplane
D.T. Jones
(
1960
)
A one-dimensional theory of liquid-fuel rocket combustion 3 the effect of non-uniform droplet radii, injection velocities and physical properties
J. Adler
(
1960
)
Stagnation-point heat-transfer rate measurements in the unexpanded flow of the N.P.L. hypersonic shock tunnel
B. D. Henshall
(
1960
)
Crack propagation in sheet material - some conclusions deduced from a combination of theory and experiment
D. Williams
(
1960
)
Now showing items 2361-2380 of 2786
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