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Aeronautical Research Council: Recent submissions
Now showing items 2201-2220 of 2786
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Free-flight measurements of the dynamic longitudinal-stability characteristics of a wind tunnel interference model (M = 0.92 to 1.35)
G. H. Greenwood
(
1963
)
Measurements in flight of the longitudinal stability derivatives of a 60 degrees delta wing aircraft (Fairey Delta 2)
D.R. Andrews
(
1959
)
The effect of skin taper on the aeroelastic properties of wings
J. A. Rein
(
1961
)
Low speed wind tunnel tests on a kite balloon model
M. H. Simonds
(
1963
)
On axial load diffusion into a thin-walled reinforced cylindrical shell
E.H. Mansfield
(
1963
)
Non-equilibrium flow of a polyatomic gas through a normal shock wave
P. A. Blythe
(
1962
)
On Three-Dimensional Bodies of Delta Planform which can Support Plane Attached Shock Waves
D. H. Peckham
(
1963
)
This Note collects together in one report available theoretical work on bodies which can support attached plane shock waves, discusses some of the possible merits of such shapes, and includes some calculations illustrating ...
Pressure measurements at supersonic speeds on three uncambered conical wings of unit aspect ratio
J. W. Britton
(
1962
)
Three-dimensional turbulent boundary layers
J. C. Cooke
(
1963
)
Surface pressures and structural strains resulting from fluctuations in the turbulent boundary layer of a fairey delta 2 aircraft
D. R. B. Webb
;
A. R. Keeler
;
G. R. Allen
(
1962
)
Atomic recombination in nozzles methods of analysis for flows with complicated chemistry
K. N. C. Bray
;
J. P. Appleton
(
1963
)
Equilibrium real-gas performance charts for a hypersonic shock-tube wind-tunnel employing nitrogen
L. Bernstein
(
1963
)
Theoretical comparison of the flow over a flat delta wing and a rectangular pyramid
E. Eminton
(
1963
)
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
)
Now showing items 2201-2220 of 2786
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