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Aeronautical Research Council: Recent submissions
Now showing items 2441-2460 of 2786
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Real gas effects on shock-tube performance at high shock strengths
J. L. Stollery
(
1958
)
Wing flow measurements of the damping in pitch derivative of a 45 degrees delta wing-body combination and with a tailplane in two positions
R. Rose
(
1957
)
Some Notes on the Use of Resistance Thermometers for the Measurement of Heat Transfer Rates in Shock Tubes
B. D. Henshall
;
D. L. Schultz
(
1959
)
A method of calculating the effect of one helicopter rotor upon another
I. C. Cheeseman
(
1958
)
The theoretical performances of shock tubes designed to produce high shock speeds
B. D. Henshall
(
1958
)
The influence of a model on plenum chamber indication of mach number in a slotted wall wind tunnel
L.C. Squire
;
A. Stanbrook
(
1958
)
Some methods of evaluating imperfect gas effects in aerodynamic problems
G. A. Bird
(
1958
)
Numerical aspects of unsteady lifting-surface theory at supersonic speeds
H. C. Garner
(
1958
)
List of current papers published for the Aeronautical Research Council (numbers 351-400)
Aeronautical Research Council
(
1962
)
A technique for improving the predictions of linearised theory on the drag of straight-edged wings
D. G. Randall
(
1958
)
The longitudinal response of an aircraft with auto-pilot, including an incidence term in the height control equation
M. R. Watts
;
D. E. Fry
(
1958
)
Automatic data reduction equipment for wind tunnels
G. C. Rowley
(
1958
)
High reynolds number tests on a 70 degrees L.E. sweepback delta wing and body (H.P. 100) in the compressed air tunnel
R. W. F. Gould
;
C. F. Cowdrey
(
1958
)
Some contributions to jet-flap theory and to the theory of source-flow from aerofoils
L. C. Woods
(
1958
)
Complex variable applications to certain coupled systems
D. P. Jenkins
(
1958
)
Some details of the quintic profile for use in the polhausen-type of boundary-layer calculation
N. Curle
(
1958
)
Development and flight tests of an instrument flight director for helicopters
P. Brotherhood
(
1958
)
Multi-channel slip rings for stress and temperature measurement
R. Chaplin
(
1958
)
A shock-expansion theory applicable to wings with attached shock waves
L.M. Sheppard
;
K.D. Thomson
(
1958
)
Some results of an investigation into the use of air injection in a model of the diffuser for the A.R.A. supersonic tunnel
E. C. Carter
;
K. F. Tucker
(
1958
)
Now showing items 2441-2460 of 2786
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