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Showing 10 out of a total of 462 results for community: Aeronautical Research Council.
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Comparison between dynamic stability boundaries for NPL 9615 and NACA 0012 aerofoils pitching about the quarter-chord
A. W. Moore
;
N. C. Lambourne
;
L. Woodgate
(
1974
)
Pressures near the centre-line of Leeward surfaces on delta wings and conical bodies at high supersonic speeds
M. J. Larcombe
(
1971
)
Decay of trailing vortices
E. H. Oon
(
1973
)
Low-speed wind-tunnel measurements of surface pressure fluctuations on two slender-wing models
D. A. Lovell
;
T. B. Owen
(
1971
)
List of Current Papers published for the Aeronautical Research Council. Nos. 1101-1150
Unknown author
(
1972
)
Subsonic theoretical lift-curve slope, aerodynamic centre and spanwise loading for arbitrary aspect ratio, taper ratio and sweepback
H. C. Garner
;
Sandra M. Inch
(
1971
)
The nature, development and effect of the viscous flow around an aerofoil with high-lift devices
D. N. Foster
;
P. R. Ashill
;
B. R. Williams
(
1974
)
A novel method for the estimation of the zero-lift forebody pressure drag of axisymmetric non-slender shapes at supersonic and hypersonic velocities
P. G. Pugh
;
L. C. Ward
(
1971
)
The characteristics of a family of rooftop aerofoils designed at their drag-rise condition in viscous, compressible flow part 1 design condition
B. G. J. Thompson
;
S. W. Cosby
(
1975
)
The design and aerodynamic characteristics of the RAE 5215 aerofoil
P. G. Wilby
(
1977
)
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F. E. Kiddle (10)
D. G. Mabey (8)
H. C. Garner (8)
J. Weber (8)
E. H. Mansfield (7)
D. R. Gaukroger (6)
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C. C. L. Sells (5)
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