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On the static thrust of contra-rotating airscrews
Collar, A. R.
(
H. M. Stationery Office
,
1941
)
Porous Properties of Various Materials liable to be used for Making Parachutes
W. D. Brown
;
M.Sc.
;
A.M.I.Mech.E.
;
J. F. Holford
(
1949
)
Photographs of shock wave movement
W. F. Hilton
;
R. G. Fowler
(
1947
)
Wind-tunnel tests on the spoiling effects of engine cooling gills on radial air-cooled installations on a wing
J. Seddon
;
J. A. Kirk
(
1942
)
Flight tests at high mach number on E28/39 W4041 (single-engined jet-propelled aircraft)
A. W. Thom
;
F. Smith
;
J. Brotherton
(
1945
)
High-speed tunnel tests of a 5 per cent. Chord dive-recovery flap on a NACA 0015 aerofoil
D. A. Clarke
(
1948
)
Wing parachutes for recovery from the spin. Part I - General design requirements. Part II - Wake Phenomena.
G. E. Pringle
;
T. V. Somerville
;
D. J. Harper
;
J. R. Mitchell
;
J. Picken
;
G. E. Pringle
(
1947
)
The high-speed laboratory of the aerodynamics Division, N.P.L. Part I - description of the installation. Part II - experimental techniques. Part III - experimental results.
D. W. Holder
(
1946
)
Low-speed measurements of the pressure distribution at the surface of a swept-back wing
V. M. Falkner
;
Doris E. Lehrian
(
1949
)
An aerofoil designed to give laminar flow over the whole surface with boundary-layer suction
E. J. Richards
;
C. H. Burge
(
1943
)
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A. D. Young (8)
V. M. Falkner (8)
J. H. Preston (7)
W. P. Jones (7)
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E. H. Mansfield (5)
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equations (1)
fluid properties (1)
hydrodynamics (1)
lateral stability (1)
rudder (1)
yawing moments (1)
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1949 (51)
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