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AERADE: Recent submissions
Now showing items 2601-2620 of 3498
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Computer programmes to calculate the response of flexible aircraft to gusts and control movements
C. G. B. Mitchell
(
1967
)
Free-flight measurements of the incremental drag due to engine nacelles on a transonic swept-wing aircraft
G. K. Hunt
(
1967
)
Measurements of drag, base pressure and base aerodynamic heat transfer appropriate to 8.5 degrees semi-angle sharp cones in free flight at mach numbers from 0.8 to 3.8
G. H. Greenwood
(
1967
)
Nitrogen condensation in the R.A.R.D.E. hypersonic gun tunnel
J. E. Bowman
(
1967
)
List of current papers (numbers 901-950)
Aeronautical Research Council
(
1967
)
Measurements of wing buffeting on a scimitar model
D. G. Mabey
(
1967
)
The thermal assessment of personal conditioning garments
D. R. Burton
(
1967
)
Some theoretical studies concerning oleo damping characteristics
H. Hall
(
1967
)
Crack propagation tests on 2024-T3 unstiffened aluminium alloy panels of various length-width ratios
T. J. Carter
(
1967
)
The accuracy of pressure transducers when used in short-duration wind tunnel facilities
L. Pennelegion
;
K. Wilson
;
B. Redston
(
1967
)
Measurements at transonic speeds of the sideforce and yawing moment on various store arrangements mounted beneath a 45 degrees swept wing-fuselage model
P. Marsden
;
A.B. Haines
(
1964
)
A convenient representation of creep strain data for problems involving time-varying stresses and temperatures
J. M. Clarke
(
1967
)
A note on the design and construction of a low-pressure calibrator and a comparison with shock-tube and static calibration methods
R. J. Pallant
(
1967
)
Wind tunnel tests on a rectangular, twin duct, variable geometry air intake at supersonic speeds
M. D. Dobson
(
1967
)
A turbulent skin-friction law for use at subsonic and transonic speeds
J. F. Nash
;
A. G. J. Macdonald
(
1967
)
An analogue computer for on-line correction of wind tunnel force and moment data
B. E. Pecover
(
1967
)
Tests with a two-dimensional intake having all-external compression and a design mach number of 2.2
M. C. Neale
;
P. S. Lamb
(
1967
)
A theoretical investigation of the effect of aspect ratio on axial flow compressor performance
J. H. Horlock
;
G. J. Fahmi
(
1967
)
Tests with a two-dimensional intake having all-external compression and a design mach number of 2.0
M. C. Neale
;
P. S. Lamb
(
1967
)
Project topcat power spectral measurements of clear air turbulence associated with jet streams
Anne Burns
;
C. K. Rider
(
1967
)
Now showing items 2601-2620 of 3498
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