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Aeronautical Research Council Current Papers: Recent submissions
Now showing items 1041-1060 of 1393
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Calculated aerodynamic forces on a sweptback untapered wing oscillating in incompressible flow
D. L. Woodcock
(
1958
)
Static and dynamic response of a design of differential pressure yawmeter at supersonic speeds
L. J. Beecham
;
S. J. Collins
(
1958
)
A note on the interpretation of base pressure measurements in supersonic flows
R. C. Hastings
(
1958
)
Low-speed wind-tunnel tests of the effects of various leading-edge modifications on the sectional characteristics of a thin wing (6 per cent thick, R.A.E. 101 section)
S.F.J. Butler
(
1958
)
Critical flight conditions and loads resulting from inertia cross-coupling and aerodynamic stability deficiencies
W. J. G. Pinsker
(
1958
)
A flight technique for the measurement of thrust boundaries and of drag due to lift
H. D. Rylands
(
1958
)
Static response of a hemispherical-headed yawmeter at high subsonic and transonic speeds
P.G. Hutton
(
1958
)
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
)
Now showing items 1041-1060 of 1393
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