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AERADE: Recent submissions
Now showing items 2801-2820 of 3498
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On the variation of profile drag coefficient below the critical mach number
J. F. Nash
;
T. H. Moulden
;
J. Osborne
(
1964
)
Tests on a hunter F.2 of two strain gauge methods for measuring tailplane loads in flight, with some loads measured in level flight, pitch-ups and transonic dives
O.P. Nicholas
(
1964
)
A collection of data on the lift-dependent drag of uncambered slender wings at supersonic speeds
A.L. Courtney
(
1964
)
A free-flight investigation of wing-body junction design for a transonic swept-wing aircraft
G. K. Hunt
(
1964
)
A parameter theory for the compressible flow through variable-area turbo-machines
Gordon S. Beavers
(
1965
)
On forward ejection for thermal insulation in hypersonic flight
M. G. Hall
(
1964
)
Simulation of ground controlled approaches with reference to certain accidents
K. J. Holden
(
1965
)
Static tests of ground effect on planforms fitted with a centrally-located round lifting jet
L. A. Wyatt
(
1964
)
Some simple calculations relating to the generation of an R.F. plasma
E. G. Broadbent
(
1964
)
A microsecond response pressure transducer for blast wave measurements
D. Pierce
(
1964
)
Wind tunnel tests at M = 2.0 on interference effects between intake flows in a four-engine nacelle
M. D. Dobson
(
1964
)
A theoretical approach to air bag shock absorber design
A.C. Browning
(
1964
)
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
)
Now showing items 2801-2820 of 3498
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