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Aeronautical Research Council Current Papers: Recent submissions
Now showing items 821-840 of 1393
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A preliminary study of ionic recombination of argon in wind-tunnel nozzles part 2
K. N. C. Bray
;
J. A. Wilson
(
1963
)
Tabulated solutions of the equilibrium gas properties behind the incident and reflected normal shock-wave in a shock-tube 1 nitrogen 2 oxygen
L. Bernstein
(
1963
)
The calibration of a 60 degrees cone to measure mach number, total pressure and flow angles at supersonic speeds
D. R. Andrews
;
W. G. Sawyer
(
1962
)
Aerodynamic and mechanical tests of a model of a variable mach number nozzle
Z. M. Jawor
(
1963
)
Some characteristics of rectangular multi-shock and isentropic external compression intakes at a mach number of 2.9
R. A. Dutton
;
E. L. Goldsmith
(
1961
)
The use of dust deposition as a means of flow visualisation
E. T. Hignett
(
1962
)
An investigation of wing-aileron flutter using ground launched rocket models
D. R. Gaukroger
;
J. K. Curran
(
1962
)
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
)
Now showing items 821-840 of 1393
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