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Aeronautical Research Council: Recent submissions
Now showing items 1601-1620 of 2786
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The effect of leading-edge geometry on high-speed stalling
G. F. Moss
;
A. B. Haines
;
R. Jordan
(
1973
)
Similarity requirements for aeroelastic models of helicopter rotors
G. K. Hunt
(
1973
)
List of current papers (numbers 1201-1250)
Aeronautical Research Council
(
1973
)
Measurement of the Internal Performance of a Rectangular Air Intake having Variable Geometry Compression Surfaces at Mach Numbers from 1.7 to 2.5. Part 11 The Effect of Incidence
C. S. Brown
;
E. L. Goldsmith
(
1973
)
Measurements have been made of the internal performance of a rectangular intake having variable geometry compression surfaces. The measurements have been made within a range of Mach numbers from 1.7 to 2.46 and at angles ...
On the calibration of pressure transducers for use in shock-tunnels
R. O. Goodchild
;
L. Bernstein
(
1973
)
Measurement of the internal performance of a rectangular air intake with variable geometry at mach numbers from 1.7 to 2.5 part 1
C. S. Brown
;
E. L. Goldsmith
(
1973
)
Comparative turbulence for a Canberra and a vulcan flying together at low altitude
J. K. Curran
(
1973
)
The calculated growth of lift and moment on a swept wing entering a discrete vertical gust at subsonic speeds
H. C. Garner
(
1973
)
Some aerodynamic considerations of the flight characteristics of towing systems using long towlines at high speeds
D. Pierce
;
L. J. Beecham
(
1972
)
Decay of trailing vortices
E. H. Oon
(
1973
)
Plane turbulent jet flow in a favourable pressure gradient
M. J. Riley
(
1973
)
On the effects of viscous interaction for a flat delta wing at incidence
L. Davies
(
1973
)
Measurements of temperature and pressure behind the incident and reflected shocks in a shock tube
Michael J. Lewis
;
Leonard Bernstein
(
1973
)
The measurement and analysis of the profile drag of a wing with a slotted flap
I. R. M. Moir
;
D. N. Foster
;
D. R. Holt
(
1972
)
The off-design analysis of flow in axial compressors
H. Daneshyar
;
M. R. A. Shaalan
(
1972
)
Design development of an aircraft strut in carbon fibre reinforced plastic
T. A. Collings
(
1972
)
Aerodynamic data for the BAC 221 up to a mach number of 0.955 as measured in wind tunnel tests
Dorothy M. Holford
(
1972
)
A review of wind tunnel tests on circulation-control devices for aircraft control
F. G. Maccabee
;
B. R. Hilton
;
J. I. Marsh
(
1972
)
Low speed pull-up manoeuvres for a slender wing transport aircraft with stability and control augmentation
Dorothy M. Holford
(
1972
)
The longitudinal stability characteristics of an ogee wing of slenderness ratio = 0.35
A. G. Hepworth
(
1972
)
Now showing items 1601-1620 of 2786
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