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AERADE: Recent submissions
Now showing items 2721-2740 of 3498
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Interim report on low-speed flight tests of a slender-wing research aircraft (Handley-page H.P.115)
P. L. Bisgood
;
C. O. O'Leary
(
1966
)
Handling qualities of aircraft with marginal longitudinal stability
T.B. Saunders
(
1966
)
Comparison of seven wing buffet boundaries measured in wind tunnels and in flight
D. G. Mabey
(
1966
)
The interpretation of strain measurements for flight load determination
P. B. Hovell
;
D. A. Webber
;
T. A. Roberts
(
1966
)
An experimental check on the theoretical relationship between the spectral density and the probability distribution of crossings for a stationary random process with Gaussian distribution, using data obtained in measurements of aircraft response to turbul
J. Burnham
(
1965
)
Preston tube measurements in turbulent boundary layers and fully developed pipe flow
D. H. Ferriss
(
1965
)
Review of general operating experience with a jet-lift VTOL research aircraft (short S.C.1)
D. Lean
;
H. W. Chinn
(
1965
)
A survey of aircraft handling criteria
C. Leyman
;
E. R. Nuttall
(
1966
)
Turbulent-boundary-layer behaviour and the auxiliary equation
John F. Nash
(
1966
)
A unified theory of friction, heat transfer and mass transfer in the turbulent boundary layer and wall jet
D. B. Spalding
(
1965
)
Slender-body theory calculations of the effect on lift and moment of mounting the wing off the fuselage centre-line
R. S. Bartlett
(
1965
)
Further tests with a variable ramp intake having a design mach number of 2.2
M. C. Neale
;
P. S. Lamb
(
1966
)
The time required for high speed airstreams to disintegrate water drops
D. C. Jenkins
;
J. D. Booker
(
1965
)
Measurements of vortex-breakdown position at low speed on a series of sharp-edged symmetrical models
P. B. Earnshaw
(
1965
)
Experimental investigation of the breakdown of a vortex in a tube
D. L. I. Kirkpatrick
(
1965
)
A digital recording system for structural research
D. Purslow
(
1965
)
The static pressure distribution around a circular jet exhausting normally from a plane wall into an airstream
L. J. S. Bradbury
;
M. N. Wood
(
1965
)
A parametric study of take-off and landing distances for high-lift aircraft
W. A. Mair
;
B. J. Edwards
(
1965
)
Analysis of flight loads recorded on comet 4B aircraft by means of the fatigue load meter
R. Hain Taylor
(
1965
)
Measurements of dynamic stability from three simplified free-flight models of a supersonic research aircraft (Bristol T.188) over the mach number range 1.2 - 2.6
K. J. Turner
(
1965
)
Now showing items 2721-2740 of 3498
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