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Aeronautical Research Council: Recent submissions
Now showing items 2101-2120 of 2786
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List of current papers (numbers 701-750)
Aeronautical Research Council
(
1965
)
Measurements of zero-lift drag at supersonic speeds for a symmetrical slender-wing model with different roughness bands
E. C. Carter
(
1964
)
The influence of gas streams and magnetic fields on electric discharges part 1 arcs at atmospheric pressure in annular gaps
V. W. Adams
(
1964
)
A theoretical survey of the potentialities of insulation and internal cooling for alleviation of steady kinetic heating
D. J. McCue
(
1964
)
Wind tunnel force and moment investigation at M = 4.3 into the application of various devices for the control of a cone-cylinder-flare configuration
B. E. Pecover
(
1964
)
Use of a wind tunnel to determine the performance of slender wings suitable for a supersonic transport aircraft
J. Y. G. Evans
(
1964
)
8 ft x 8 ft tunnel tests on a model of the de havilland 'blue streak'
G. F. Moss
;
D. Isaacs
(
1964
)
Experimental evidence on the drag at zero lift on a series of slender delta wings at supersonic speeds, and the drag penalty due to distributed roughness
M.C.P. Firmin
(
1964
)
Theoretical stability derivatives for a symmetrically tapered wing at low supersonic speeds
Doris E. Lehrian
;
Gillian Smart
(
1965
)
Flight measurements at subsonic speeds of the aileron rolling power and lateral stability derivatives lv and yv on a 60 degree delta wing aircraft (Fairey Delta 2)
F. W. Dee
(
1964
)
Roughness criteria and drag penalties for bands of distributed roughness on two slender wings at supersonic speeds
D. G. Mabey
(
1964
)
8 ft x 6 ft tunnel tests on a model of the De Havilland "blue streak" at mach numbers of 0.80 to 1.25
A.L. Courtney
(
1964
)
Some notes on turbulent boundary layers with fluid injection at high supersonic speeds
L. C. Squire
(
1964
)
Free-flight tests of vortex generator configurations at transonic speeds
J.B.W. Edwards
(
1966
)
The addition of peripheral vision to the artificial horizon
K. J. Holden
(
1964
)
Wind tunnel measurements of the unsteady pressures in and behind a bomb bay (Canberra)
J. E. Rossiter
;
A. G. Kurn
(
1965
)
The effects of high pressure on the flow in the reflected shock tunnel
L. Davies et al
(
1964
)
Wind tunnel measurements of normal force and pitching moment at a mach number of 2.00 on a 1:30 scale model of blue streak
E. Huntley
(
1964
)
Power spectra of low level atmospheric turbulence measured from an aircraft
A. Burns
(
1964
)
Simple theoretical and experimental studies of the flow through a three-shock system in a corner
E. Eminton
(
1966
)
Now showing items 2101-2120 of 2786
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