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Aeronautical Research Council: Recent submissions
Now showing items 2221-2240 of 2786
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Pressure measurements on a cone-cylinder-flare configuration at small incidences for M
J. G. Woodley
(
1963
)
The estimation of oscillatory wing and control derivatives
W. E. A. Acum
;
H. C. Garner
(
1964
)
Notes on some experimental and theoretical results for the boundary layer development aft of the shock in a shock-tube
L. Bernstein
(
1963
)
Qualitative solutions of the stability equation for a boundary layer in contact with various forms of flexible surface
T. Nonweiler
(
1963
)
Measurements of transient pressures on a narrow-delta wing due to an upward gust
G. K. Hunt
;
D. R. Roberts
;
D. Walker
(
1964
)
The calculation of transient temperatures in turbine blades and tapered discs using biot's variational method
P. W. H. Howe
(
1961
)
Comparative thrust measurements on a series of jet-flap configurations and circular nozzles
M. N. Wood
(
1962
)
A comparison of two methods for predicting the potential flow around arbitrary airfoils in cascade
D. Pollard
;
J. Wordsworth
(
1962
)
Tests to high subsonic speeds in the 10 ft x 7 ft tunnel, of several wing-mounted air-brakes on a half-model of a four-jet bomber vickers valiant
M. J. Richards
;
D. J. Harper
(
1963
)
The construction and testing of a large axial flow compressor
R. Shaw
;
A. Lewkowicz
(
1962
)
A theoretical investigation of the effect of change in axial velocity on the potential flow through a cascade of aerofoils
D. Pollard
;
J. H. Horlock
(
1963
)
A consideration of the similarity requirements for aerothermoelastic tests on reduced scale models
W. G. Molyneux
(
1962
)
Diffraction of oblique shock wave
R. S. Srivastava
(
1962
)
Determination of ion density and temperature of a water-stabilised arc from observations of the line profiles of the hydrogen lines H beta and H gamma
P. S. Pusey
;
K. C. Lapworth
;
A. F. Metherell
(
1963
)
Laminar mixing of a non-uniform stream with a fluid at rest
J. F. Nash
(
1962
)
The testing and development of a ground muffler for jet engine exhaust noise
D. Middleton
(
1961
)
Flow field and pressure distribution measurements on blunt-nosed bodies at M = 6.8 parts 1 and 2
W. K. Osborne
;
J. F. W. Crane
(
1961
)
The equilibrium piston technique for gun tunnel operation
R. A. East
;
L. Pennelegion
(
1962
)
An investigation of two methods of suppressing shock oscillation ahead of conical centre-body intakes
C. F. Griggs
(
1962
)
A crude theory of hovercraft performance at zero tilt
S. B. Gates
(
1961
)
Now showing items 2221-2240 of 2786
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