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Showing 10 out of a total of 367 results for collection: Aeronautical Research Council Reports & Memoranda.
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Measurement of the pitching-moment derivatives for rigid tapered wings of hexagonal planform oscillating in supersonic flow
L. Woodgate
;
J. F. M. Maybrey
;
C. Scruton
(
1961
)
Alleviation of leading-edge heating by conduction and radiation
E. C. Capey
(
1966
)
Published reports and memoranda of the Aeronautical Research Council
Unknown author
(
1962
)
Tests at transonic speeds on wings with wedge sections and sweep varying between 0 degree and 60 degrees
E. W. E. Rogers
;
C. J. Berry
;
V. G. Quincey
(
1961
)
Mechanical Aspects of Turbine Blade Cooling Part I. Description of an Experimental High-Temperature Turbine and Associated Test Rig (Cooled Turbine No. 126) Part II. The Behaviour of Extruded Air-Cooled Rotor Blades Subjected to Steady High Temperature an
N.E. Waldren
;
et al
(
1962
)
A three component gun tunnel balance designed for testing thin delta wings
T. Opatowski
(
1969
)
An experimental and theoretical comparison at M=4 of the lift-to-drag ratio of some possible aircraft shapes
C. S. Brown
;
E. L. Goldsmith
(
1967
)
Resonance tests on a Beagle B206 Series 1 aircraft
F. J. Hawkins
;
R. F. Mousley
(
1966
)
The theoretical treatment of slowly oscillating part-span control surfaces in subsonic flow
H. C. Garner
;
Doris E. Lehrian
(
1969
)
Take-off tests on a transport aircraft including the use of a 'SCAT' take-off director
C. O. O'Leary
;
J. N. Cannell
;
R. L. Maltby
(
1966
)
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E. W. E. Rogers (9)
H. C. Garner (8)
C. J. Berry (7)
D. E. Davies (7)
W. J. G. Pinsker (7)
D. S. Whitehead (6)
Doris E. Lehrian (6)
G. G. Pope (6)
P. Bradshaw (6)
A. J. Sobey (5)
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1969 (28)
1968 (29)
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1964 (37)
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